Garmin | G1000: Quest Kodiak 100 | Garmin G1000: Quest Kodiak 100 G1000 Cockpit Reference Guide for Quest Kodiak 100

Garmin G1000: Quest Kodiak 100 G1000 Cockpit Reference Guide for Quest Kodiak 100
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Quest KODIAK® 100
FLIGHT INSTRUMENTS
ENGINE INDICATING SYSTEM
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2007-2010, 2012, 2014-2015 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0552.23 or later for the Quest
KODIAK 100. Some differences in operation may be observed when comparing the information
in this manual to earlier or later software versions.
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Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
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and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
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Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®
and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be
used without the express permission of Garmin.
KODIAK® is a registered trademark of Quest Aircraft Company; NavData® is a registered
trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications.
Honeywell® and Bendix/King® are registered trademarks of Honeywell International, Inc.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with respect to the AC-U-KWIK information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK
Organizations do not warrant or make any representations regarding its accuracy, reliability, or
otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent
allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of
action, claims or losses related to any actual or alleged inaccuracies in the information arising
out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to licensee.
July, 2015
190-00645-08 Rev. A
Printed in the U.S.A.
Warnings, Cautions & Notes
WARNING: Navigation and terrain separation must NOT be predicated upon
the use of the terrain avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74B Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in
the G1000 system must be updated regularly in order to ensure that the
information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Warnings, Cautions & Notes
WARNING: Do not use data link weather products (e.g., XM WX Satellite
Weather, GFDS Worldwide Weather, or FIS-B) for hazardous weather
penetration. Weather information provided by these products is aged by
up to several minutes and may not depict actual weather conditions as they
currently appear.
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.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Warnings, Cautions & Notes
WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
WARNING: Lamp(s) inside this product may contain mercury (HG) and must
be recycled or disposed of according to local, state, or federal laws. For
more information, refer to our website at www.garmin.com/aboutGarmin/
environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the
system within the following areas could result in loss of reliable attitude and
heading indications. North of 72° North latitude at all longitudes. South of
70° South latitude at all longitudes. North of 65° North latitude between
longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude
between longitude 70° W and 128° W. (Northern Canada). North of 70° North
latitude between longitude 85° E and 114° E. (Northern Russia). South of
55° South latitude between longitude 120° E and 165° E. (Region south of
Australia and New Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are
derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Warnings, Cautions & Notes
CAUTION: The PFD and MFD displays use a lens coated with a special
anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive
cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTIREFLECTIVE 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 antireflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifications could void both the warranty and the
pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen
images of the G1000 panel and displays, are subject to change and may not
reflect the most current G1000 system and aviation databases. Depictions
of equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: 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: 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
190-00645-08 Rev. A
Warnings, Cautions & Notes
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a
resource with which to more easily find operating instructions on the major
features of the G1000 system. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Pilot’s Guide for this aircraft.
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory
and advisory guidance and information related to the use of databases in
the National Airspace System.
• Garmin equipment will only recognize and use databases that are
obtained from Garmin or Jeppesen. Databases obtained from Garmin
or Jeppesen are assured compliance with all data quality requirements
(DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A
copy of the Type 2 LOA is available for each database and can be viewed
at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to
operate in accordance with established AFM(S) and regulatory guidance or
limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Warnings, Cautions & Notes
NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support to coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes;
or any other displayed item used for navigation or communication in the air
or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data
Error Report.’
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Record of Revisions
Part Number
190-00645-00
190-00645-01
190-00645-02
190-00645-03
190-00645-04
Rev A
190-00645-05
190-00645-06
190-00645-08 Rev. A
Change Summary
Initial release
Added Airways, WAAS, VNAV, and Charts
Added Synthetic Vision System
Updated G1000 System Messages
Added other GDU 9.03 parameters
Added AOPA Airport Directory
Added dual navigation database capability
Added database synchronization
Added flight plan import/export
Added new user waypoint creation procedure
Added other GDU 10.01 parameters
Added TKS anti-icing CAS alerts
Updated Ice Protection display on the Engine System Page
Updated CAS messages
Added GDU 12.01 parameters
Added GWX 68 support
Added GTS 800 support
Updated CAS messages
Added GDU 14.01 parameters
Added Garmin AFCS
Added Garmin ESP
Added Maintenance Log feature
Added AC-U-KWIK Airport Directory
Added User Defined Holding Patterns
Added temperature compensated altitude
Changed XM to SiriusXM
Changed Synthetic Vision System (SVS) to Synthetic Vision Technology
(SVT)
Added Weather Radar Overlay
Added Profile View
Updated System Messages
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
RR-1
Record of Revisions
Part Number
190-00645-07
190-00645-08
Change Summary
Corrected Underspeed Protection CAS Warning
Added AFCS Config CAS Warning
Updated System Software Number
Updated Warnings, Cautions, and Notes
Updated Warning Alerts
Updated Annunciation Advisories
Revision Date of Revision Affected Pages
A
July, 2015
All
RR-2
Description
Production Release
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Table of Contents
Flight Instruments........................................................................................................................ 1
Displaying the Metric Altitude Overlay................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Synchronizing the Altimeter Barometric Pressure Settings............................................ 1
Setting the Baro Transition Alert........................................................................................... 2
Changing the HSI Display Format.......................................................................................... 2
Changing the Navigation Angle True/Magnetic Setting................................................... 2
Selecting Bearing Display and Changing Sources.............................................................. 2
Synchronizing the CDIs............................................................................................................. 3
Changing the Selected GPS CDI Setting............................................................................... 3
Change Navigation Sources.................................................................................................... 3
Enabling/Disabling OBS Mode While Navigating with GPS.............................................. 3
Displaying Wind Data............................................................................................................... 4
Generic Timer.............................................................................................................................. 4
Changing Vspeeds and Turning Bugs On/Off....................................................................... 4
Enabling/Disabling All Vspeed Bugs...................................................................................... 5
Restoring All Vspeed Defaults................................................................................................ 5
Set Barometric Minimum Descent Altitude......................................................................... 5
Engine Indication System......................................................................................................... 7
Engine Display............................................................................................................................ 7
Engine System Display............................................................................................................. 8
Engine Fuel Display................................................................................................................... 9
Nav/Com/Transponder/Audio Panel.................................................................................. 11
Enter a Transponder Code..................................................................................................... 11
Selecting a COM Radio........................................................................................................... 11
Selecting a NAV Radio............................................................................................................ 11
NAV/COM Tuning...................................................................................................................... 11
Digital Clearance Recorder and Player............................................................................... 12
Intercom System (ICS) Isolation........................................................................................... 13
Automatic Flight Control System...................................................................................... 15
Flight Director Activation...................................................................................................... 15
Vertical Modes.......................................................................................................................... 16
Lateral Modes........................................................................................................................... 17
Flap Configuration Trim (FCT)............................................................................................... 18
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
i
Table of Contents
GPS Navigation............................................................................................................................ 19
Direct-to Navigation............................................................................................................... 19
Activate a Stored Flight Plan................................................................................................ 20
Activate a Flight Plan Leg...................................................................................................... 20
Stop Navigating a Flight Plan............................................................................................... 21
Vertical Navigation (VNAV)................................................................................................... 21
Flight Planning............................................................................................................................. 25
Weight Planning....................................................................................................................... 25
Trip Planning............................................................................................................................. 25
Create a User Waypoint Defined by Latitude & Longitude............................................ 27
Create a User Waypoint Defined by Radials from Other Waypoints............................ 28
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 30
Create a User Waypoint using the Map Pointer............................................................... 31
Delete a User Waypoint.......................................................................................................... 32
Create a Flight Plan................................................................................................................. 32
Import a Flight Plan from an SD Card................................................................................. 33
Insert a Waypoint in the Active Flight Plan....................................................................... 34
Enter an Airway in a Flight Plan........................................................................................... 35
Creating a User-Defined Hold at an Active Flight Plan Waypoint................................. 35
Creating a User-Defined Hold at the Aircraft Present Position..................................... 36
Creating a User-Defined Hold At A Direct-To Waypoint.................................................. 37
Exiting a User-Defined Hold Inserted Into The Active Flight Plan................................ 37
Removing a User-Defined Hold Inserted Into The Active Flight Plan.......................... 37
Removing a User-Defined Hold At An Off-Route Direct-To............................................ 38
Invert an Active Flight Plan................................................................................................... 38
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 38
Store a Flight Plan................................................................................................................... 39
Edit a Stored Flight Plan........................................................................................................ 39
Delete a Waypoint from the Flight Plan............................................................................. 39
Invert and Activate a Stored Flight Plan............................................................................ 40
Copy a Flight Plan.................................................................................................................... 40
Delete a Flight Plan................................................................................................................. 40
Graphical Flight Plan Creation.............................................................................................. 41
Export a Flight Plan to an SD Card...................................................................................... 41
Procedures...................................................................................................................................... 43
Load and Activate a Departure Procedure........................................................................ 43
Activate A Departure Leg...................................................................................................... 43
Load An Arrival Procedure..................................................................................................... 43
Activate An Arrival Leg.......................................................................................................... 44
Load and/or Activate an Approach Procedure.................................................................. 44
Activate An Approach in the Active Flight Plan................................................................ 45
ii
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Table of Contents
Activate a Vector to Final Approach Fix............................................................................. 46
Activate A Missed Approach in the Active Flight Plan.................................................... 46
Temperature Compensated Altitude................................................................................... 46
Hazard Avoidance....................................................................................................................... 49
Customizing the Hazard Displays on the Navigation Map............................................. 49
STORMSCOPE® (Optional)...................................................................................................... 49
SiriusXM Weather (Optional)................................................................................................ 51
Traffic Systems......................................................................................................................... 54
Terrain Awareness & Warning System (TAWS) Display.................................................... 58
Airborne Color Weather Radar (Optional)......................................................................... 59
Profile View Terrain................................................................................................................. 63
Additional Features................................................................................................................... 65
Synthetic Vision Technology (SVT)....................................................................................... 65
Terminal Procedure Charts.................................................................................................... 66
Airport Directory..................................................................................................................... 68
SiriusXM Radio Entertainment (Optional)......................................................................... 69
Maintenance Logs.................................................................................................................... 71
Scheduler................................................................................................................................... 72
Electronic Checklists............................................................................................................... 74
Auxiliary Video......................................................................................................................... 75
Electronic Stability & Protection (ESP™)............................................................................. 77
Abnormal Operation................................................................................................................. 79
Reversionary Mode................................................................................................................. 79
Abnormal COM Operation..................................................................................................... 79
Hazard Displays with Loss of GPS Position........................................................................ 79
Unusual Attitudes.................................................................................................................... 80
Dead Reckoning....................................................................................................................... 80
Annunciations & Alerts............................................................................................................ 83
Aircraft Alerts........................................................................................................................... 83
Aural Alerts............................................................................................................................... 85
Comparator Annunciations.................................................................................................... 86
Reversionary Sensor Annunciations.................................................................................... 87
AFCS Alerts................................................................................................................................ 88
TAWS-B Alerts........................................................................................................................... 89
TAWS-B System Status Annunciations................................................................................ 90
MFD & PFD Message Advisories........................................................................................... 90
Database Message Advisories.............................................................................................. 92
GMA 1347 Message Advisories............................................................................................. 96
GIA 63W Message Advisories................................................................................................ 97
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
iii
Table of Contents
GEA 71 Message Advisories................................................................................................. 100
GTX 33 Message Advisories................................................................................................. 101
GRS 77 Message Advisories................................................................................................. 101
GMU 44 Message Advisories............................................................................................... 103
GWX 68 Message Advisories............................................................................................... 104
GDL 69A/69A SXM Message Advisories............................................................................ 104
GDC 74A Message Advisories.............................................................................................. 105
GMC 710 Message Advisories............................................................................................. 105
GTS 800 Message Advisories............................................................................................... 106
Miscellaneous Message Advisories.................................................................................... 106
Flight Plan Import/Export Messages................................................................................. 110
Pilot Profile Import/Export Messages............................................................................... 112
Appendix........................................................................................................................................ 113
PFD Softkey Map................................................................................................................... 113
MFD Softkey Map.................................................................................................................. 119
Updating Databases.............................................................................................................. 121
iv
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
DISPLAYING THE METRIC ALTITUDE OVERLAY
2)
Press the ALT UNIT Softkey.
3)
Press the METERS Softkey to turn on metric altitude readouts.
4)
Press the BACK Softkey to return to the top-level softkeys.
Nav/Com/
XPDR/Audio
Press the PFD Softkey to display the second-level softkeys.
EIS
1)
AFCS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
GPS Nav
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the STD BARO Softkey.
Flight
Planning
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Hazard
Avoidance
1)
Procedures
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
Additional
Features
Or:
4)
Abnormal
Operation
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION
Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
5)
Press the FMS Knob to remove the cursor.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
Select the AUX-SYSTEM SETUP Page on the MFD using the FMS Knob.
Appendix
1)
Annun/
Alerts
SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS
1
Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight Altitude in the Baro Transition Alert
box.
4)
Turn the small FMS Knob to turn the alert OFF or ON and press the ENT
Key.
5)
Turn the small FMS Knob to change the altitude and press the ENT Key.
6)
To cancel the selection, press the FMS Knob.
CHANGING THE HSI DISPLAY FORMAT
1)
Press the PFD Softkey
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI or ARC HSI Softkey.
CHANGING THE NAVIGATION ANGLE TRUE/MAGNETIC SETTING
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
1)
EIS
SETTING THE BARO TRANSITION ALERT
Nav/Com/
XPDR/Audio
Flight
Instruments
Flight Instruments
1)
Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight Nav Angle in the Display Units box.
4)
Turn the small FMS Knob to highlight the desired setting and press the
ENT Key.
• MAGNETIC - Angles corrected to the computed magnetic variation (Mag
Var)
SELECTING BEARING DISPLAY AND CHANGING SOURCES
Index
Appendix
Annun/
Alerts
Abnormal
Operation
• TRUE - References angles to true north (T)
2
1)
Press the PFD Softkey.
2)
Press a BRG Softkey to display the desired bearing pointer and information
window with a NAV source.
3)
Press the BRG Softkey again to change the bearing source to GPS.
4)
To remove the bearing pointer and information window, press the BRG
Softkey again.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Instruments
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window.
4)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
Nav/Com/
XPDR/Audio
Select the AUX - SYSTEM SETUP Page using the FMS Knob on the MFD.
EIS
1)
Flight
Instruments
SYNCHRONIZING THE CDIS
CHANGING THE SELECTED GPS CDI SETTING
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight Selected in the GPS CDI box.
4)
Turn the small FMS Knob to highlight the desired setting and press the
ENT Key.
5)
To cancel the selection, press the FMS Knob or the CLR Key.
Flight
Planning
2)
GPS Nav
Use the FMS Knob to select the AUX - SYSTEM SETUP Page on the MFD.
AFCS
1)
CHANGE NAVIGATION SOURCES
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or
LOC2. This places the cyan tuning box over the NAV2 standby frequency.
3)
Press the CDI Softkey a third time to return to GPS.
Additional
Features
2)
Hazard
Avoidance
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the cyan tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
Procedures
1)
Abnormal
Operation
ENABLING/DISABLING OBS MODE WHILE NAVIGATING WITH GPS
2)
Turn the CRS Knob to select the desired course to/from the waypoint. Press
a CRS Knob to synchronize the Selected Course with the bearing to the
next waypoint.
3)
Press the OBS Softkey again to return to automatic waypoint sequencing.
Appendix
Press the OBS Softkey to select OBS Mode.
Annun/
Alerts
1)
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
3
DISPLAYING WIND DATA
EIS
Flight
Instruments
Flight Instruments
1)
Press the PFD Softkey.
2)
Press the WIND Softkey to display wind data to the left of the HSI.
3)
Press one of the OPTN softkeys to change how wind data is displayed:
Nav/Com/
XPDR/Audio
• OPTN 1: Headwind/tailwind and crosswind arrows with numeric speed
components
AFCS
• OPTN 2: Wind direction arrow with numeric headwind (H) or tailwind (T)
and crosswind (X) speed components
• OPTN 3: Wind direction arrow with true numeric direction and speed
Procedures
Hazard
Avoidance
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it will start counting UP after reaching zero). Press the
CLR Key or the TMR/REF Softkey to remove the window.
CHANGING VSPEEDS AND TURNING BUGS ON/OFF
Abnormal
Operation
Additional
Features
To remove the window, press the OFF Softkey.
GENERIC TIMER
Flight
Planning
GPS Nav
4)
Annun/
Alerts
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Index
Appendix
speed has been changed from a default value, an asterisk appears next to
the speed).
4
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Instruments
2)
Press the MENU Key.
3)
To activate all Vspeed flags, press the ENT Key with All References On
highlighted.
4)
To remove all Vspeed flags, turn the FMS Knob to highlight All References
Off and press the ENT Key.
Nav/Com/
XPDR/Audio
Press the TMR/REF Softkey.
EIS
1)
Flight
Instruments
ENABLING/DISABLING ALL VSPEED BUGS
Press the TMR/REF Softkey.
2)
Press the MENU key.
3)
Turn the FMS Knob to highlight Restore Defaults and press the ENT key.
GPS Nav
1)
AFCS
RESTORING ALL VSPEED DEFAULTS
Flight
Planning
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
Procedures
1) Press the TMR/REF Softkey.
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select the desired altitude source: barometric
(BARO) or temperature compensated (TEMP COMP). OFF is selected by
default. Press the ENT Key or turn the large FMS Knob to highlight the
next field.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet).
5)
To remove the window, press the CLR Key or press the TMR/REF Softkey.
Hazard
Avoidance
2)
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
5
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
Blank Page
6
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Engine Indication System
Flight
Instruments
ENGINE INDICATION SYSTEM
ENGINE DISPLAY
AFCS
Engine
Torque
GPS Nav
Inlet Turbine
Temperature
Flight
Planning
Propeller
RPM
Procedures
Gas Generator
RPM
Fuel Flow(pounds
per hour)
Oil Pressure
Indicator
Hazard
Avoidance
Oil Temperature
Indicator
Nav/Com/
XPDR/Audio
Pressing the ENGINE Softkey makes available the SYSTEM and FUEL softkeys
which in turn provide access to the System Display and the Fuel Display, respectively.
EIS
In all cases, green indicates normal operation, yellow indicates caution, and red
indicates warning.
Additional
Features
Ammeter
Flap Position
Voltmeter
Abnormal
Operation
Fuel Quantity
Indicator
Elevator Trim
Aileron and
Rudder Trim
Annun/
Alerts
Default Engine Display
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
7
ENGINE SYSTEM DISPLAY
1)
Press the ENGINE Softkey.
2)
Press the SYSTEM Softkey.
3)
To return to the default Engine Display, press the ENGINE or BACK
Softkey.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
Index
Appendix
Annun/
Alerts
SYSTEM Engine Display
8
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Engine Indication System
Press the ENGINE Softkey.
2)
Press the FUEL Softkey.
3)
To return to the default Engine Display, press the ENGINE or BACK
Softkey.
EIS
1)
Flight
Instruments
ENGINE FUEL DISPLAY
AFCS
• DEC FUEL – Decreases totalizer-based fuel remaining in 10-lb increments
Nav/Com/
XPDR/Audio
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.
• INC FUEL – Increases totalizer-based fuel remaining in 10-lb increments
GPS Nav
• RST FUEL – Resets totalizer-based fuel remaining to the aircraft’s fuel capacity
and the displayed fuel used (LB USED) to zero
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
FUEL Engine Display
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
9
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
Blank Page
10
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER A TRANSPONDER CODE
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
GPS Nav
SELECTING A COM RADIO
Transmit/Receive
Flight
Planning
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
SELECTING A NAV RADIO
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
2)
Appendix
Press the small tuning knob to select the desired radio for tuning. A cyan
box highlights the radio frequency to be tuned.
Annun/
Alerts
NAV/COM TUNING
Abnormal
Operation
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
Additional
Features
1)
Hazard
Avoidance
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
Procedures
Receive Only
1)
AFCS
2)
Nav/Com/
XPDR/Audio
Press the XPDR Softkey to display the transponder mode selection softkeys.
EIS
1)
11
DIGITAL CLEARANCE RECORDER AND PLAYER
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
• 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 begins playing the next
previously recorded block.
12
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Nav/Com/XPDR/Audio Panel
Press the PILOT and/or COPLT Key on either audio panel to select those isolated
from hearing the Nav/Com radios and music.
Flight
Instruments
INTERCOM SYSTEM (ICS) ISOLATION
EIS
Annun/
Alerts
Passengers,
Music
Abnormal
Operation
Appendix
ON
Selected
Selected
Radios,
Radios, Aural
Passengers,
Aural
Alerts, Pilot,
Music
Alerts, Pilot,
Copilot
Copilot
Additional
Features
ON
ON
Selected
Radios,
Aural Alerts,
Copilot
Hazard
Avoidance
OFF
Selected
Radios, Aural
Alerts, Pilot,
Passengers,
Music
Procedures
OFF
Flight
Planning
ON
GPS Nav
OFF
Selected
Radios,
Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Selected
Radios,
Selected
Aural Alerts,
Radios, Aural
Copilot,
Alerts, Pilot
Passengers,
Music
Selected
Radios, Aural
Alerts, Pilot,
Copilot,
Passengers,
Music
Copilot
Pilot Side
Side
Passenger
Passenger
Hears
Hears
Selected
Selected
Radios,
Radios,
Aural
Aural
Alerts, Pilot, Alerts, Pilot,
Copilot,
Copilot,
Passengers, Passengers,
Music
Music
Selected
Radios,
Copilot,
Aural Alerts,
Passengers,
Copilot,
Music
Passengers,
Music
Selected
Radios,
Aural
Passengers,
Alerts, Pilot, Pilot, Music
Passengers,
Music
AFCS
OFF
Copilot
Hears
Nav/Com/
XPDR/Audio
PILOT KEY COPLT KEY
Pilot Hears
Annunciator Annunciator
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
13
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
14
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
AFCS
Modes Selected
HDG Key
Heading Select
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Appendix
Approach**
PIT
Annun/
Alerts
APR Key
Pitch Hold (default)
Abnormal
Operation
Backcourse***
PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight
director.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
15
Index
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV or APR Key press activates flight director.
190-00645-08 Rev. A
Additional
Features
BC Key
Pitch Hold (default)
Hazard
Avoidance
Navigation**
GA Switch
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
GPS
VOR
LOC
HDG
Procedures
NAV Key
FD Key
AP Key
CWS Button
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
TO
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Takeoff (on ground)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
Control Pressed
AFCS
FLIGHT DIRECTOR ACTIVATION
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Nav/Com/
XPDR/Audio
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EIS
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
VERTICAL MODES
Vertical Mode
Pitch Hold
Selected Altitude
Capture
Altitude Hold
Flight Level Change,
IAS Hold
Vertical Path Tracking
VNV Target Altitude
Capture
Glidepath
Takeoff
Go Around
Index
Appendix
Abnormal
Operation
Glideslope
Annun/
Alerts
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Vertical Speed
Level
Description
Control Annunciation
Holds the current aircraft pitch
attitude; may be used to climb/ (default)
descend to the Selected Altitude
PIT
Captures the Selected Altitude
ALTS
*
Holds the current Altitude Reference ALT Key ALT nnnnn ft
Maintains the current aircraft
vertical speed; may be used to climb/ VS Key VS nnnn fpm
descend to the Selected Altitude
Maintains the current aircraft
airspeed while the aircraft is
FLC Key FLC nnn kt
climbing/descending to the Selected
Altitude
Captures and tracks descent legs of VNV
VPTH
an active vertical profile
Key
Captures the Vertical Navigation
**
ALTV
(VNV) Target Altitude
Captures and tracks the WAAS
GP
glidepath on approach
APR Key
Captures and tracks the ILS
GS
glideslope on approach
Commands a constant pitch angle
and wings level on the ground in
TO
GA
preparation for takeoff
Switch
Commands a constant pitch angle
GA
and wings level in the air
LVL
Commands a zero degree pitch
LVL
angle and wings level
Button
* ALTS armed automatically when PIT, VS, FLC, TO, or GA active, and under VPTH when Selected
Altitude is to be captured instead of VNV Target Altitude
** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of
Selected Altitude
16
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
AFCS
Lateral Mode
Roll Hold
GPS
VOR
Flight
Planning
LOC
Procedures
BC
Hazard
Avoidance
Approach, GPS
HDG
GPS Nav
Navigation, GPS **
Navigation, VOR Enroute
Captures and tracks the
Capture/Track **
selected navigation source NAV Key
Navigation, LOC Capture/ (GPS, VOR, LOC)
Track
(No Glideslope)
Captures and tracks a
Backcourse Capture/Track localizer signal for backcourse BC Key
approaches
*
AFCS
Heading Select **
ROL
Nav/Com/
XPDR/Audio
Low Bank
Annunciation
EIS
Description
Control
Holds the current aircraft roll
attitude or rolls the wings level,
(default)
depending on the commanded
bank angle
Limits
the
maximum BANK
commanded roll angle
Key
Captures and tracks the
HDG Key
Selected Heading
GPS
Captures and tracks the
selected navigation source APR Key
(GPS, VOR, LOC)
VAPP
Additional
Features
LOC
Abnormal
Operation
Approach, VOR Capture/
Track
Approach, LOC Capture/
Track
(Glideslope Mode
automatically armed)
Flight
Instruments
LATERAL MODES
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
17
Lateral Mode
Takeoff
EIS
Flight
Instruments
AFCS
Level
Annunciation
TO
GA
LVL
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in
green along the Roll Scale of the Attitude Indicator.
** The Heading, Navigation GPS, and Navigation VOR mode maximum roll command limit will be
limited to the Low Bank mode value if it is engaged.
FLAP CONFIGURATION TRIM (FCT)
The Flap Configuration Trim (FCT) feature automatically adjusts Pitch Trim when
flap settings are changed. FCT becomes operational when the aircraft is in the air,
autopilot is disengaged, and the flap setting is more than 2 degrees. FCT can be inhibited
by pressing and holding the AP DISC Switch. FCT will again become active when the
AP DISC Switch is released.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Go Around
Description
Control
Commands a constant pitch
angle and wings level on the
GA
ground in preparation for takeoff
Switch
Commands a constant pitch
angle and wings level in the air
LVL
Commands wings level with
zero degree pitch angle
Button
18
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
2)
3)
6)
9)
12)
1)
2)
5)
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
19
Index
6)
Appendix
4)
).
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
) Key.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EIS
Direct-to Navigation from the MFD
EIS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the OFFSET distance field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key and turn the small FMS Knob to display the Flight Plan
Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Press the ACT LEG Softkey.
3)
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
4)
With ‘Activate’ highlighted, press the ENT Key.
Index
Appendix
OR
20
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This will not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION (VNAV)
AFCS
GPS Nav
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EIS
1)
Flight
Planning
Procedures
Large White
Text
Large Cyan
Text
Hazard
Avoidance
Small Cyan
Text
Additional
Features
Small Cyan
Subdued Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
21
Since altitudes loaded with an arrival procedure are published only for turbojet
aircraft, the altitudes are displayed as white text indicating that the altitudes are
displayed for reference only. An arrival waypoint altitude may be used (or “designated”)
as is, or changed to a different altitude. An altitude is designated by pressing the FMS
Knob and turning the large FMS Knob to place the cursor on the desired altitude and
pressing the ENT Key, or by entering a different value and pressing the ENT Key. The
altitude is now displayed as blue text, indicating that the altitude is now designated to
give vertical speed and deviation guidance.
Approach waypoint altitude constraints are designated in the same way as
previously described for arrivals. These altitudes are also displayed as blue text after
being designated for use. Waypoint altitude constraints may be designated up to, but
not including the FAF. The FAF is always a “reference only” altitude and cannot be
designated, unless the selected approach does not provide vertical guidance. In this
case, the FAF altitude can be designated.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
22
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
GPS Navigation
Cyan Text
Cyan Subdued
Text
Large Text Altitude calculated by
the system estimating
the altitude of the
aircraft as it passes
over the navigation
point. This altitude
is provided as a
reference and is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
entered by the pilot.
Altitude is designated
for use in giving
vertical flight path
guidance. Altitude
does not match the
published altitude in
navigation database or
no published altitude
exists.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text Altitude is not
designated to be used
in determining vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
and is provided as a
reference.
Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches
a published altitude
in the navigation
database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Flight
Instruments
White Text
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
23
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
Blank Page
24
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT PLANNING
EIS
All procedures apply to the MFD unless otherwise stated.
Entering Weight Parameters
Procedures
3)
Press the FOB SYNC Softkey to enter the fuel on board quantity as read
from the aircraft fuel quantity sensors.
Additional
Features
Turn the large FMS Knob to place the cursor in the ‘FUEL ON BOARD’ field.
Or:
Annun/
Alerts
Press the FMS Knob to remove the cursor.
Abnormal
Operation
Manually enter the desired fuel quantity.
6)
Hazard
Avoidance
2)
Enter the desired reserve fuel quantity.
Flight
Planning
If necessary, press the FMS Knob to activate the cursor.
5)
GPS Nav
1)
Press the ENT Key. The cursor is now in the ‘FUEL RESERVES’ field.
AFCS
Entering Fuel Parameters
4)
Nav/Com/
XPDR/Audio
The Weight Planning Page is displayed after system power-up. If it is necessary to
return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the
small FMS Knob to select the Weight Planning Page.
1) Press the EMPTY WT Softkey to place the cursor in the Basic Empty Weight
field.
2) Enter the desired aircraft empty weight.
3) Press the ENT Key. The cursor is now over the ‘PILOT & STORES’ field.
4) Enter the desired weight of Pilot & Stores.
5) Press the ENT Key.
6) Continue repeating these steps until all desired weights have been entered.
TRIP PLANNING
Appendix
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the Trip Planning Page.
3)
The current page mode is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
25
Index
1)
Flight Planning
Flight
Instruments
4)
For Direct-to planning:
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
EIS
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Nav/Com/
XPDR/Audio
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
AFCS
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
GPS Nav
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Flight
Planning
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
Procedures
d) Press the ENT Key to accept the waypoint.
Or:
Hazard
Avoidance
For flight plan leg planning:
a) Press the FPL Softkey (at the bottom of the display).
Additional
Features
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
Annun/
Alerts
Abnormal
Operation
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
d) Turn the small 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’ displays the 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.
Appendix
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Index
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.
26
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
8)
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
9)
The flashing cursor moves to the fuel onboard field. Modify the fuel onboard.
Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is
provided by the entry made on the Weight Planning Page.
Hazard
Avoidance
Additional
Features
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
Procedures
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
Flight
Planning
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
GPS Nav
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
AFCS
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Nav/Com/
XPDR/Audio
7)
EIS
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Flight
Instruments
6)
Abnormal
Operation
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
Annun/
Alerts
1)
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
27
Flight Planning
Flight
Instruments
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
EIS
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Nav/Com/
XPDR/Audio
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
1)
Turn the large FMS Knob on the Control Unit to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
7)
AFCS
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
Abnormal
Operation
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Appendix
Annun/
Alerts
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Index
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
28
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
b) Turn the large FMS Knob to select the desired waypoint.
EIS
c) Press the ENT Key.
Flight
Instruments
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Or:
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
d) Press the ENT Key.
AFCS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Or:
Procedures
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
12) Press the ENT Key.
Annun/
Alerts
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Abnormal
Operation
d) Press the ENT Key.
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
Or:
13) Repeat step 10 to enter the next waypoint name.
Index
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Appendix
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
29
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
1)
Turn the large FMS Knob on the MFD Control Unit to select the ‘WPT’ page
group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Flight
Planning
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Hazard
Avoidance
Procedures
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
7)
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
Additional
Features
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
Abnormal
Operation
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Annun/
Alerts
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
30
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Flight
Instruments
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
EIS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
AFCS
d) Press the ENT Key.
Or:
GPS Nav
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Flight
Planning
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Hazard
Avoidance
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Additional
Features
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
2)
Press the ENT Key. The User Waypoint Information Page is displayed with
the captured position.
Annun/
Alerts
Press the Joystick to activate the panning function and pan to the map
location of the desired user waypoint.
Abnormal
Operation
CREATE A USER WAYPOINT USING THE MAP POINTER
1)
31
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Appendix
NOTE: If the pointer has highlighted a map database feature, one of three
things happens upon pressing the ENT Key: 1) information about the selected
feature is displayed instead of initiating a new waypoint, 2) a menu pops up
allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or
3) a new waypoint is initiated with the default name being the selected map
item.
190-00645-08 Rev. A
Procedures
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Enter a user waypoint name (up to six characters).
4)
Press the ENT Key to accept the selected name.
5)
If desired, define the type and location (i.e., LAT/LON, RAD/RAD or RAD/
DIS) of the waypoint.
6)
Press the ENT Key to accept the new waypoint.
7)
If desired, change the storage method of the waypoint to ‘TEMPORARY‘ or
‘NORMAL‘ by moving the cursor to ‘TEMPORARY‘ and selecting the ENT
Key to check or uncheck the box.
8)
Press the FMS Knob to remove the flashing cursor.
9)
Press the GO BACK Softkey to return to the map page.
Procedures
Hazard
Avoidance
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
5)
Turn the small FMS Knob to highlight the desired waypoint.
6)
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
CREATE A FLIGHT PLAN
Abnormal
Operation
Additional
Features
3)
DELETE A USER WAYPOINT
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Index
Appendix
Annun/
Alerts
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
32
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6)
When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the IMPORT Softkey.
Appendix
4)
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
33
Index
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
190-00645-08 Rev. A
Annun/
Alerts
Turn the small FMS Knob to select the Flight Plan Catalog Page.
Abnormal
Operation
3)
Additional
Features
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
Hazard
Avoidance
2)
Procedures
Insert the SD card containing the flight plan in the top card slot on the
MFD.
Flight
Planning
1)
GPS Nav
IMPORT A FLIGHT PLAN FROM AN SD CARD
AFCS
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
Nav/Com/
XPDR/Audio
5)
EIS
Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
Flight
Instruments
4)
Flight Planning
Flight
Instruments
Or:
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
If an existing flight plan is selected, an ‘Overwrite existing flight plan? OK
or CANCEL’ prompt is displayed. Press the ENT Key to choose to overwrite
the selected flight plan and see a list of the available flight plans on the SD
card. If overwriting the existing flight plan is not desired, select ‘CANCEL’
using the FMS Knob, press the ENT Key, select another existing or empty
flight plan, and again press the IMPORT Softkey.
1)
Press the FPL Key to display the active flight plan.
2)
If required, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5)
Enter the new flight plan waypoint by one of the following:
Hazard
Avoidance
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
Additional
Features
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Abnormal
Operation
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
Annun/
Alerts
d) Press the ENT Key.
Or:
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Index
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
34
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Flight
Instruments
d) Press the ENT Key.
e) Press the ENT Key again to accept the waypoint.
Or:
c) Turn the large FMS Knob to select the desired user waypoint.
d) Press the ENT Key.
Press the ENT Key again to “accept” the waypoint.
AFCS
6)
GPS Nav
ENTER AN AIRWAY IN A FLIGHT PLAN
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey, or press the MENU Key and select ‘Load Airway‘. The Select Airway
Page is displayed. The LD AIRWY Softkey or the ‘Load Airway‘ menu
item is available only when an acceptable airway entry waypoint has been
chosen (the waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
Annun/
Alerts
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
Index
1)
Appendix
CREATING A USER-DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Abnormal
Operation
3)
Additional
Features
Press the FMS Knob to activate the cursor (not required on the PFD).
Hazard
Avoidance
2)
Procedures
Press the FPL Key.
Flight
Planning
1)
190-00645-08 Rev. A
Nav/Com/
XPDR/Audio
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
EIS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
35
3)
Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The
HOLD AT window appears with the course field highlighted.
4)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
CREATING A USER-DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
36
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the course field highlighted.
3)
If desired, use the FMS Knobs to edit the entry course, and press the ENT
Key.
4)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
5)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
6)
Use the FMS Knobs to edit the length, and press the ENT Key.
7)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
8)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
9)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to create an Offroute
Direct-to hold waypoint and activate the hold.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Flight
Instruments
CREATING A USER-DEFINED HOLD AT A DIRECT-TO WAYPOINT
Press a Direct-to Key and set up the direct-to waypoint as desired, but
select ‘HOLD?’ instead of ‘ACTIVATE?’ when finished (MFD or PFD).
2)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
3)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
4)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
5)
Use the FMS Knobs to edit the length, and press the ENT Key.
6)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
7)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
8)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the direct-to
with the user-defined hold defined at the direct-to waypoint. (If the directto wayoint is part of the active flight plan, the HOLD is inserted into the
active flight plan. If the direct-to waypoint is not part of the active flight
plan, an off-route direct-to hold is created.
EIS
1)
AFCS
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
Annun/
Alerts
1)
Abnormal
Operation
REMOVING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT PLAN
Appendix
37
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
GPS Nav
Press the SUSP Softkey. The system will provide guidance to follow the
holding pattern to the inbound course and resume automatic waypoint
sequencing.
190-00645-08 Rev. A
Nav/Com/
XPDR/Audio
EXITING A USER-DEFINED HOLD INSERTED INTO THE ACTIVE FLIGHT PLAN
REMOVING A USER-DEFINED HOLD AT AN OFF-ROUTE DIRECT-TO
1)
Press a Direct To Key to display the DIRECT TO Window (PFD or MFD).
2)
Press the MENU Key to display the PAGE MENU with the cursor on the
‘Cancel Direct-To NAV’ selection.
3)
Press the ENT Key. The holding pattern is removed.
INVERT AN ACTIVE FLIGHT PLAN
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
1)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or:
a) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Additional
Features
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
2)
Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
3)
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
d) Press the EDIT Softkey.
38
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
GPS Nav
Press the FPL Key and turn the small FMS Knob to display the Flight Plan
Catalog Page.
Flight
Planning
Or, for a stored flight plan:
b) Press the FMS Knob to activate the cursor.
Abnormal
Operation
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Press the EDIT Softkey.
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the
cursor.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
39
Index
3)
Appendix
Turn the large FMS Knob to highlight the waypoint to be deleted.
Annun/
Alerts
2)
190-00645-08 Rev. A
Additional
Features
a) Press the FPL Key on the MFD, then turn the small FMS Knob to select
the Flight Plan Catalog Page.
Hazard
Avoidance
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Procedures
DELETE A WAYPOINT FROM THE FLIGHT PLAN
1)
AFCS
1)
Nav/Com/
XPDR/Audio
EDIT A STORED FLIGHT PLAN
EIS
1)
Flight
Instruments
STORE A FLIGHT PLAN
INVERT AND ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
Press the FPL Key.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
DELETE A FLIGHT PLAN
1)
Press the FPL Key.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
1)
Flight
Planning
COPY A FLIGHT PLAN
Procedures
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
40
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Flight Planning
Flight
Instruments
GRAPHICAL FLIGHT PLAN CREATION
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Press the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
EXPORT A FLIGHT PLAN TO AN SD CARD
Press the FPL Key on the Control Unit to display the Active Flight Plan Page
on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
Additional
Features
2)
Hazard
Avoidance
Insert the SD card into the top card slot on the MFD.
Procedures
1)
Flight
Planning
3)
GPS Nav
Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
AFCS
2)
Nav/Com/
XPDR/Audio
Press the FPL Key on the MFD to display the Active Flight Plan Page.
EIS
1)
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
41
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Blank Page
42
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EIS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
Hazard
Avoidance
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
LOAD AN ARRIVAL PROCEDURE
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Appendix
1)
43
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Procedures
ACTIVATE A DEPARTURE LEG
190-00645-08 Rev. A
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival becomes part of the active flight plan.
ACTIVATE AN ARRIVAL LEG
Procedures
Flight
Planning
GPS Nav
Turn the large FMS Knob to highlight the desired arrival.
1)
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Additional
Features
Hazard
Avoidance
4)
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
44
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Procedures
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO or
optional TEMP COMP.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
13) Press the ENT Key.
Abnormal
Operation
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Appendix
Press the PROC Key.
Annun/
Alerts
1)
Additional
Features
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and is immediately
activated.
Hazard
Avoidance
12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Procedures
11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
Flight
Planning
10) Press the ENT Key. If BARO or OFF was selected in step 8, proceed to step
11. If TEMP COMP was selected in step 8, the cursor moves to the ‘TEMP
AT....” field. Turn the small FMS Knob to enter the temperature at the
destination airport. The temperature compensated altitude minimum is
displayed below the previously enter minimum altitude value.
GPS Nav
8)
AFCS
Press the ENT Key. The cursor moves to the MINIMUMS field.
Nav/Com/
XPDR/Audio
7)
EIS
Turn either FMS Knob to select the desired transition. 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.
Flight
Instruments
6)
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
45
ACTIVATE A VECTOR TO FINAL APPROACH FIX
GPS Nav
Flight
Planning
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
5)
After activating the missed approach procedure, and the CDI has changed
to TERM mode sensitivity, another approach procedure may be loaded.
TEMPERATURE COMPENSATED ALTITUDE
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
1)
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
Annun/
Alerts
Altitudes Displayed Without
Temperature Compensation
Altitudes Displayed With
Temperature Compensation
Index
Appendix
Enabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
46
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Procedures
Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4)
Use the small FMS Knob to select the temperature at the <airport>. The
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
Nav/Com/
XPDR/Audio
5)
EIS
compensated altitude is computed as the temperature is selected.
shown in the flight plan.
AFCS
Disabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
GPS Nav
Press the ENT Key. The temperature compensated altitude at the FAF
Procedures
is cancelled.
Flight
Planning
5)
Flight
Instruments
3)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
47
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
Blank Page
48
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
EIS
1)
AFCS
Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Annun/
Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Appendix
Selecting the ‘cell’ or ‘strike’ mode on the Navigation Map
Press the MENU Key.
2)
With ‘Map Setup’ selected, press the ENT Key.
3)
Select the ‘Weather’ group.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
1)
Additional
Features
2)
Hazard
Avoidance
Press the MAP Softkey.
Procedures
1)
Flight
Planning
Displaying Stormscope Lightning Data on the Navigation Map Page
GPS Nav
WARNING: Do not rely on information from a lightning detection system display
as the sole basis for hazardous weather avoidance. Range limitations and
interference may cause the system to display inaccurate or incomplete information.
Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
Lightning Age
Strike is less than 6 seconds old
Nav/Com/
XPDR/Audio
STORMSCOPE® (OPTIONAL)
49
4)
Press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’.
5)
Turn the large FMS Knob to select ‘STRMSCP MODE’.
6)
Turn the small FMS Knob to change between ‘CELL’ and ‘STRIKE’ options.
When an item is selected, press the ENT Key.
7)
Press the FMS knob to return to the Navigation Map Page.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
AFCS
Manually Clearing Stormscope Lightning Data on the Navigation Map
1)
Press the MENU Key.
2)
Select ‘Clear Stormscope Lightning®’.
3)
Press the ENT Key.
GPS Nav
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
Flight
Planning
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.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Selecting a Stormscope range on the Navigation Map
1)
Press the MENU Key.
2)
Select ‘MAP SETUP’.
3)
Select the ‘Weather’ group.
4)
Press the ENT Key.
5)
Turn the large FMS Knob to select ‘STRMSCP SMBL’.
6)
Turn the small FMS Knob to select the maximum display range.
7)
Press the ENT Key.
8)
Press the FMS Knob to return to the Navigation Map Page.
Appendix
Annun/
Alerts
Stormscope Page
1)
Turn the large FMS Knob until the Map Page group is selected.
2)
Turn the small FMS Knob until the Stormscope Page is selected.
3)
To change the map range, turn the Joystick clockwise to zoom out or
counter-clockwise to zoom in.
Index
Changing between ‘cell’ and ‘strike’ mode on the Stormscope Page
50
1)
Select the Stormscope Page.
2)
Press the MODE Softkey. The CELL and STRIKE softkeys are displayed.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to
display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box in the
upper left corner of the Stormscope Page.
4)
Press the BACK Softkey to return to the main Stormscope page.
EIS
Change the Viewing Mode Between 360˚ and 120˚
2)
Press the VIEW Softkey. The 360 and ARC softkeys are displayed. Press the
360 Softkey to display a 360˚ viewing area or press the ARC Softkey to
display a 120˚ viewing area.
3)
Press the BACK Softkey to return to the main Stormscope page.
GPS Nav
SIRIUSXM WEATHER (OPTIONAL)
Abnormal
Operation
Annun/
Alerts
Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press the applicable softkey again to remove weather data from the
Navigation Map Page.
Display METAR and TAF information on the Airport Information Page
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
Turn the large FMS Knob to select the WPT Page Group.
Appendix
1)
Additional
Features
2)
Hazard
Avoidance
Displaying SiriusXM Weather on the Navigation Map Page
Procedures
WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be significantly older than the indicated weather
product age.
Flight
Planning
WARNING: Do not use data link weather information for maneuvering in, near,
or around areas of hazardous weather. Information contained within data link
weather products may not accurately depict current weather conditions.
Press the MAP Softkey.
AFCS
Select the Stormscope Page.
Nav/Com/
XPDR/Audio
1)
1)
Flight
Instruments
3)
51
Hazard Avoidance
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Weather on the Weather Data Link Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Select the available softkeys to select the desired SiriusXM Weather product.
4)
Press the LEGEND Softkey to view the legends for the selected products. If
necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
GPS Nav
AFCS
Map Panning Information – Weather Data Link Page
1)
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
SIGMETs, PIREPs or AIREPs.
3)
Press the ENT Key to display pertinent information for the selected product.
Hazard
Avoidance
Procedures
Flight
Planning
Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and 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.
NOTE: NEXRAD data cannot be displayed at the same time as terrain, echo
tops, turbulence, or icing data is displayed.
Additional
Features
SiriusXM Weather Products and Symbols
Abnormal
Operation
Wx Product
Status Icons
Description
Annun/
Alerts
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
Appendix
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.
Index
SiriusXM LIGHTNING - The age of the displayed data is shown at the right.
52
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
CELL MOVEMENT - The age of the displayed data is shown at the right.
EIS
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Additional
Features
AIREP - The age of the displayed data is shown at the right.
Abnormal
Operation
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
Annun/
Alerts
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
Appendix
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
No Status Icon
Hazard
Avoidance
CYCLONE WARNING - The age of the displayed data is shown at the right.
Procedures
COUNTY WARNING - The age of the displayed data is shown at the right.
Flight
Planning
WINDS ALOFT - Available for the US and Canada. The age of the displayed
data for each is shown at the right. The altitude selection is shown at the
bottom.
GPS Nav
FREEZING LEVEL - The age of the displayed data is shown at the right.
AFCS
SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.
Nav/Com/
XPDR/Audio
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
TFR- Depicted as an area outlined in yellow
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
53
TRAFFIC SYSTEMS
• If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and
TNA MUTE Softkey is displayed.
• If a Traffic Advisory System (TAS) is configured, a STANDBY, OPERATE, TEST,
and ALT MODE Softkey is displayed.
Traffic Symbol
Description
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Proximity Advisory (PA) (TAS only, not available with TIS)
(intruder is within 5 nm and less than 1200’ vertical separation)
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
GPS Nav
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Flight
Planning
Traffic Advisory Off Scale
Procedures
Traffic Symbol Description
Hazard
Avoidance
Traffic Information Service (TIS)
Additional
Features
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Abnormal
Operation
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Index
Appendix
Annun/
Alerts
Displaying Traffic on the Traffic Map Page
54
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
Flight
Instruments
6)
Displaying Traffic on the Navigation Map
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Nav/Com/
XPDR/Audio
Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
EIS
1)
SKY497 Traffic Advisory System (TAS) (Optional)
GPS Nav
System Self Test
Set the range to 2/6 nm.
2)
Press the STANDBY Softkey.
3)
Press the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert “Traffic Advisory
System Test Passed” is heard. If the self test fails, the system reverts to
Standby Mode and a voice alert “Traffic Advisory System Test Failed” is
heard.
Flight
Planning
1)
Press the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
5)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
4)
Appendix
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
Annun/
Alerts
3)
Abnormal
Operation
Turn the small FMS Knob to select the second rectangular page icon.
Additional
Features
2)
Hazard
Avoidance
Turn the large FMS Knob to select the Map Page Group.
Procedures
Displaying Traffic on the Traffic Map Page
1)
AFCS
NOTE: Refer to the SKY497 Pilot’s Guide for a detailed discussion of this
Traffic Advisory System (TAS).
55
Hazard Avoidance
EIS
Flight
Instruments
Displaying Traffic on the Navigation Map
1)
Ensure TAS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Nav/Com/
XPDR/Audio
GTS 800 Traffic Advisory System (TAS) (Optional)
1)
Set the range to 2/6 nm.
2)
Press the STANDBY Softkey.
3)
Press the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols display and a voice alert “Traffic Advisory
System Test Passed” is heard. If the self test fails, the system reverts to
Standby Mode and a voice alert “Traffic Advisory System Test Failed” is
heard.
Flight
Planning
GPS Nav
AFCS
System Self Test
Procedures
Enabling/Disabling Flight ID Display
On the Traffic Map Page, press the FLT ID Softkey.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the OPERATE Softkey to begin displaying traffic. OPERATING is
displayed in the Traffic mode field.
4)
Press the ALT MODE Softkey to change the altitude volume.
5)
Press the STANDBY Softkey to place the system in the Standby mode.
STANDBY is displayed in the Traffic mode field.
6)
Turn the Joystick clockwise to display a larger area or counter-clockwise to
display a smaller area.
Index
Displaying Traffic on the Navigation Map
56
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, press the MAP Softkey.
3)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
EIS
Symbol
Description
Nav/Com/
XPDR/Audio
Traffic Advisory with ADS-B directional information. Points in the direction of the intruder
aircraft track. (GTS 800 only)
Traffic Advisory without directional information.
AFCS
Traffic Advisory out of the selected display range. Displayed at outer range ring at proper
bearing.
GPS Nav
Non-threat traffic with ADS-B directional information. Points in the direction of the aircraft
track. (GTS 800 only)
Flight
Planning
Non-threat traffic with ADS-B directional information. Points in the direction of the intruder
aircraft track. (GTS 800 only)
Non-threat traffic with no directional information.
Procedures
Traffic with ADS-B directional information, but positional accuracy is degraded. Points in the
direction of the aircraft track. (GTS 800 only)
Relative Altitude
(in this case 1200
feet above own
aircraft)
Additional
Features
Altitude Trend
(up arrow
indicates
climbing, down
arrow indicates
descending)
Abnormal
Operation
Annun/
Alerts
Intruder
Aircraft
Ground Track
(extends in
the direction
of the aircraft
movement)
Hazard
Avoidance
Aircraft
Identification
(tail number
or Flight ID
number)
Flight
Instruments
NOTE: A 1090 MHz extended squitter transponder is required to display
ADS-B symbology for aircraft providing ADS-B data.
Example ADS-B Traffic Advisory (GTS 800 only)
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
57
TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
EIS
Flight
Instruments
Hazard Avoidance
Nav/Com/
XPDR/Audio
NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.
GPS Nav
AFCS
Manual System Test
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
When all is in working order, “TAWS System Test, OK” is heard.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.
4)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Display Terrain on the TAWS-B Page
Color
Terrain/Obstacle Location
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Index
Enable/Disable Aviation Data
58
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
EIS
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear on
the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
Flight
Instruments
TAWS Inhibit
Nav/Com/
XPDR/Audio
AFCS
Inhibit TAWS
While the TAWS-B Page is displayed, press the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit TAWS’.
3) Press the ENT Key.
GPS Nav
Flight
Planning
Enable TAWS
While the TAWS-B Page is displayed, press the INHIBIT Softkey.
Or:
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable TAWS’.
3) Press the ENT Key.
Procedures
Hazard
Avoidance
Additional
Features
AIRBORNE COLOR WEATHER RADAR (OPTIONAL)
Annun/
Alerts
Appendix
CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.
Abnormal
Operation
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
59
Hazard Avoidance
1)
Select the Weather Radar Page in the Map Page Group with the FMS Knob.
2)
Press the MODE Softkey.
3)
If the aircraft is on the ground, select the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar will
enter the Standby Mode. After the aircraft is airborne, select the WEATHER
Softkey.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Weather on the Weather Radar Page
Or:
4)
Turn the Joystick to select the desired map range.
5)
If desired, select the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Move the Joystick up or down to adjust the tilt of the antenna up or down.
Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
Adjusting Antenna Bearing
Move the Joystick right or left to adjust the azimuth position of the antenna right
or left. Monitor the displayed bearing value in the BEARING field.
When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Bearing Line’.
3) Press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
If the aircraft is already airborne, select the WEATHER Softkey. The oneminute warm-up period will be initiated, after which the radar will begin
transmitting.
60
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Hazard Avoidance
1) While in the Horizontal Scan view, move the Joystick to place the Bearing
Line on the desired storm cell, or other area, to be vertically scanned.
Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.
4)
Turn the Joystick to adjust the range.
5)
To select a new area to be vertically scanned, select the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.
Procedures
Select the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
2)
Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.
3)
Press the FMS Knob to remove the cursor.
4)
Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ will be
displayed in the ‘GAIN’ field.
Hazard
Avoidance
1)
Abnormal
Operation
3)
Select the BACK Softkey.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the TILT field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to display
ground returns at the desired distance.
7)
Press the FMS Knob to remove the cursor.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
Select the GROUND Softkey to place the radar in Ground Map Mode.
Appendix
2)
Annun/
Alerts
Select the MODE Softkey.
Additional
Features
Ground Mapping
1)
Flight
Planning
WARNING: Changing the gain in Weather Mode will cause precipitation
intensity to be displayed as a color not representative of the true intensity.
Remember to return the gain setting to ‘Calibrated’ for viewing the actual
intensity of precipitation.
GPS Nav
Adjusting Gain
AFCS
3)
Nav/Com/
XPDR/Audio
Select the VERTICAL Softkey. A vertical ‘slice’ of the selected area will now
be displayed.
EIS
2)
Flight
Instruments
Vertically Scan a Storm Cell
61
Hazard Avoidance
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Sector Scan
2)
Press the FMS Knob to display the cursor.
3)
Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
4)
Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.
5)
If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
6)
Press the FMS Knob to remove the cursor.
GPS Nav
Antenna Stabilization
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
will become the center point of the Sector Scan.
1)
To activate or deactivate the antenna stabilization, select the MODE
Softkey.
2)
Select the STAB ON Softkey to activate antenna stabilization or select
the STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the WATCH® feature, select the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Weather Alert
To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating
and deactivating will also enable or inhibit the alert on the PFD.
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system will automatically switch to Standby Mode.
Weather Radar Overlay on the Navigation Map Page
The Map - Weather Radar Page is the principal map page for viewing airborne
weather radar information. Weather radar information may also be shown as an
overlay on the Navigation Map Page on the MFD as an additional reference.
Index
Appendix
1)
62
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
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Hazard Avoidance
On the Navigation Map Page, press the MENU Key.
2)
With ‘Map Setup’ highlighted, press the ENT Key.
3)
Turn the small FMS Knob to select the ‘Weather’ group, then press the ENT
Key.
4)
Turn the large FMS Knob to scroll through the product selections and
highlight the WX RADAR overlay selection (‘On’ or ‘Off’). Turn the small
FMS knob to highlight the desired selection.
5)
To remove the menu, press the FMS Knob or CLR Key.
EIS
1)
AFCS
Procedures
Hazard
Avoidance
Select ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on
current state) and press the ENT Key.
2)
Select the MAP Softkey.
Abnormal
Operation
Select the Navigation Map Page.
Additional
Features
Enabling/Disabling Terrain on the Profile View
1)
Flight
Planning
Enabling/Disabling Profile View
2)
GPS Nav
The system offers a Profile View of terrain and obstacles relative to the aircraft’s
current flight path and altitude on the Navigation Map Page of the MFD. Profile View
does not provide terrain or obstacle caution or warning annunciations or voice alerts,
nor does it display potential impact points inside the Profile View.
On the Navigation Map Page, press the MENU Key.
Nav/Com/
XPDR/Audio
PROFILE VIEW TERRAIN
1)
Flight
Instruments
Enabling/Disabling Airborne Weather Radar Overlay on the Navigation Map
Page
3) Select the TERRAIN Softkey.
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
63
Hazard Avoidance
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Customizing the Profile Path display on the Navigation Map Page
1)
Select the Navigation Map Page.
2)
Press the MENU Key.
3)
With ‘Map Setup’ highlighted, press the ENT Key.
4)
Turn the small FMS Knob to select the ‘Profile’ Group and press the ENT
Key.
5)
Turn the large FMS Knob or press the ENT Key to scroll through product
selections.
6)
Turn the small FMS Knob to scroll through options (ON/OFF, range settings).
7)
8)
Press the ENT Key to select an option.
Press the FMS Knob or CLR Key to return to the Navigation Map Page with
the changed settings.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
• PROFILE PATH – Turns the display of the Profile Path on or off and sets
maximum map range at which the Profile Path is shown
64
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION TECHNOLOGY (SVT)
EIS
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVT is intended as an aid to situational
awareness only and may not provide either the accuracy or reliability upon
which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.
AFCS
Hazard
Avoidance
Additional
Features
Abnormal
Operation
2)
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
Appendix
Press the PFD Softkey.
Annun/
Alerts
Displaying SVT Terrain
1)
Procedures
Pathways
Flight Path Marker
Horizon Heading Marks
Traffic Display
Airport Signs
Runway Display
Terrain Alerting
Obstacle Alerting
Flight
Planning
•
•
•
•
•
•
•
•
GPS Nav
Synthetic Vision Technology (SVT) functionality is offered as an optional
enhancement to the G1000 Integrated Flight Deck System.
SVT is primarily comprised of a computer-generated, forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the primary flight display (PFD).
SVT offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVT enhancement to the PFD, the following feature enhancements
have been added to the PFD:
Index
190-00645-08 Rev. A
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65
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Pathways
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
AFCS
GPS Nav
Flight
Planning
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Softkey.
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiway identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR-1 Softkey removes VOR station ID,
the VOR symbol, and intersection names if within the airport plan view. Pressing the
66
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
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Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
DCLTR-2 Softkey removes the airport runway layout, unless the airport in view is part
of an active route structure. Pressing the DCLTR-3 Softkey cycles back to the original
map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
ChartView
Additional
Features
Abnormal
Operation
Press the SHW CHRT Softkey when displayed.
Hazard
Avoidance
1)
Procedures
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. The MFD depiction shows the aircraft position on the moving map in
the plan view of approach charts.
The FliteCharts database is updated on a 28-day cycle. If not updated within 180
days of the expiration date, FliteCharts will no longer function.
GPS Nav
FliteCharts®
AFCS
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database is
not updated within 70 days of the expiration date, ChartView will no longer function.
Or:
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
Annun/
Alerts
2)
Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs. Note that NOTAMS
are only available with ChartView.
Appendix
3)
Press the GO BACK Softkey to return to the previous page.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
67
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
View Charts from the Active Flight Plan Page
1)
While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Press the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
1)
While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
6)
In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Change Day/Night View
AIRPORT DIRECTORY
The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK
Airport Directory databases adds enhanced airport information when viewing airports
on the WPT-Airport Information Page.
The Airport Directory databases are revised every 56 days and offered on a
subscription basis. Check fly.garmin.com for the current database.
Index
View Airport Directory Information
1)
68
Turn the large FMS Knob to select the “WPT” page group.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Turn the small FMS Knob to select the AIRPORT INFORMATION Page.
Initially, information for the airport closest to the aircraft’s present position
is displayed.
3)
If necessary, select the INFO softkey until INFO-2 is displayed.
Flight
Instruments
2)
EIS
SIRIUSXM RADIO ENTERTAINMENT (OPTIONAL)
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed AUX - XM RADIO
Information Page.
GPS Nav
1)
AFCS
Selecting the XM Radio Page
Selecting a Category
Appendix
Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Annun/
Alerts
2)
Abnormal
Operation
While on the XM Radio Page, press the CHNL Softkey.
Additional
Features
Select an Available Channel within the Selected Category
Hazard
Avoidance
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Press the CATGRY Softkey on the XM Radio Page.
2) Press the CAT + and CAT - Softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
Procedures
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
Flight
Planning
Active Channel and Channel List
1)
Nav/Com/
XPDR/Audio
The XM® Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
69
Additional Features
Flight
Instruments
Or:
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
EIS
3)
With the desired channel highlighted, press the ENT Key.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Entering a Channel Directly
1)
While on the XM Radio Page, press the CHNL Softkey.
2)
Press the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Flight
Planning
Assigning Channel Presets
Additional
Features
Hazard
Avoidance
Procedures
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, press the PRESETS
Softkey to access the first five preset channels (PS1 - PS5).
2) Press the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.
3) Press any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
4) Press the SET Softkey on the desired channel number to save the channel
as a preset.
Annun/
Alerts
Abnormal
Operation
Adjusting Volume
1)
With the XM Radio Page displayed, select the VOL Softkey.
2)
Press the VOL Softkey to access the volume control softkeys.
3)
Press VOL + or VOL - softkeys to adjust the volume level.
Index
Appendix
Mute SiriusXM Audio
70
1)
Select the XM Radio Page or XM Information Page
2)
Select the MUTE Softkey to mute the audio. Select the MUTE Softkey
again to unmute the audio.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Nav/Com/
XPDR/Audio
The system provides recording of CAS, CMC, exceedances, and other critical aircraft
data that occur while the aircraft is on the ground or in flight. This may include, but
is not limited to, engine trend, exceedance and/or aircraft position data.
EIS
NOTE: An account must be established with Garmin Connext™ to make full
use of the Maintenance Logs feature.
Flight
Instruments
MAINTENANCE LOGS
Viewing the Maintenance Logs Page
2)
Turn the small FMS Knob to select AUX-MAINTENANCE LOGS Page.
GPS Nav
Turn the large FMS Knob to select the AUX page group.
AFCS
1)
Selecting the Desired Log Folder
While viewing the Maintenance Logs Page, press the small FMS Knob to
activate the cursor in the Folders.
2)
Turn the small FMS Knob to display the list of available folders. ‘INT’
displayed next to the folder name indicates that folder of log files is stored in
internal system memory. ‘EXT’ displayed next to a folder name indicates the
folder, and its contents are saved to the SD Card located in the bottom card
slot of the MFD.
3)
Turn either FMS Knob to select the desired folder.
4)
Press the ENT Key. The log files for the selected folder are displayed.
5)
Press the small FMS Knob to remove the cursor.
Flight
Planning
1)
Additional
Features
Abnormal
Operation
While viewing the Maintenance Logs Page, press the FMS Knob to activate
the cursor.
3)
Turn the large FMS Knob to display the list of available folders.
4)
Turn either FMS Knob to select the desired folder.
5)
Press the ENT Key.
6)
Turn the large FMS Knob to place the cursor on the ‘EXPORT’ button to the
right of the log file to be transmitted.
Appendix
2)
Annun/
Alerts
Place an SD Card in the top card slot of the MFD.
71
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Hazard
Avoidance
1)
190-00645-08 Rev. A
Procedures
Copy a Log File to an SD Card
EIS
Flight
Instruments
Additional Features
8)
Press the ENT Key. A .csv file is copied to the SD Card in top card slot of
the MFD.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Delete All Logs From a Selected Folder
1)
While viewing the Maintenance Logs Page, press the FMS Knob to activate
the cursor.
2)
Turn the large FMS Knob to display the list of available folders.
3)
Turn either FMS Knob to select the desired folder.
4)
Press the ENT Key.
5)
Press the MENU Key to display the Page Menu.
6)
Turn either FMS Knob to highlight ‘Delete All Logs In Folder’.
7)
Press the ENT Key. The Confirmation Window is displayed.
8)
With ‘YES’ highlighted, press the ENT Key.
Procedures
Delete All Logs From Internal Memory
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Press the ENT Key. The Export Log Window is displayed and the ‘OK’
Button is highlighted.
1)
While viewing the Maintenance Logs Page, press the MENU Key to display
the Page Menu.
2)
Turn either FMS Knob to highlight ‘Delete All Logs’.
3)
Press the ENT Key. The Confirmation Window is displayed.
SCHEDULER
The Scheduler feature can be used to enter and display reminder messages (e.g.,
Change Oil, Switch Fuel Tanks, or Altimeter-Transponder Check) in the Alerts
Window on the PFD. Messages can be set to display based on a specific date and time
(event), once the message timer reaches zero (one-time; default setting), or recurrently
whenever the message timer reaches zero (periodic). Message timers set to periodic
alerting automatically reset to the original timer value once the message is displayed.
When power is cycled, all messages are retained until deleted, and message timer
countdown is resumed.
Index
Appendix
7)
72
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Flight
Instruments
Entering a Scheduler Message
1) Select the AUX - Utility Page.
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the first empty scheduler message
naming field.
EIS
4)
Use the FMS Knob to enter the message text to be displayed in the Alerts
Window and press the ENT Key.
Nav/Com/
XPDR/Audio
5)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the field next to Type.
6)
Turn the small FMS Knob to select the message type:
• Periodic - Message issued each time the message timer reaches zero
8)
For periodic and one-time message, use the FMS Knob to enter the timer
value (HH:MM:SS) from which to count down and press the ENT Key.
9)
For event-based messages:
Hazard
Avoidance
Press the ENT Key again or use the large FMS Knob to move the cursor to
the next field.
b) Press the ENT Key again or use the large FMS Knob to move the cursor
to the next field.
Abnormal
Operation
c) Use the FMS Knob to enter the desired time (HH:MM) and press the
ENT Key.
Appendix
Deleting a Scheduler Message
1) Select the AUX - Utility Page.
Turn the large FMS Knob to highlight the name field of the scheduler
message to be deleted.
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
3)
Annun/
Alerts
10) Press the ENT Key again or use the large FMS Knob to move the cursor to
enter the next message.
Press the FMS Knob momentarily to activate the flashing cursor.
Additional
Features
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press
the ENT Key.
2)
Procedures
7)
Flight
Planning
• One-time - Message issued when the message timer reaches zero (default
setting)
GPS Nav
• Event - Message issued at the specified date/time
AFCS
2)
73
4)
Press the CLR Key to clear the message text. If the CLR Key is pressed
again, the message is restored.
5)
Press the ENT Key while the message line is cleared to clear the message
text.
EIS
Flight
Instruments
Additional Features
AFCS
Nav/Com/
XPDR/Audio
ELECTRONIC CHECKLISTS
The system accesses the checklists from an SD card inserted into the card slot.
If the SD card contains an invalid checklist file or no checklist, the Power-up Page
messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the
CHKLIST Softkey is not available.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Accessing and Navigating Checklists
1)
From any page on the MFD, press the CHKLIST Softkey.
2)
Turn the large FMS Knob to select the ‘GROUP’ field.
3)
Turn the small FMS Knob to select the desired procedure and press the
ENT Key.
4)
Turn the large FMS Knob to select the ‘CHECKLIST’ field.
5)
Turn the FMS Knob to select the desired checklist and press the ENT Key.
The selected checklist item is indicated with white text surrounded by a
white box.
6)
Press the ENT Key or press the CHECK Softkey to check the selected
checklist item. The line item turns green and a checkmark is placed in the
associated box. The next line item is automatically selected for checking.
Abnormal
Operation
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Index
Appendix
Annun/
Alerts
Press the CLR Key or press the UNCHECK Softkey to remove a check mark
from an item.
74
7)
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’
will be displayed in yellow text.\
8)
Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the
cursor.
9)
Press the ENT Key to advance to the next checklist.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Flight
Instruments
10) Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
Immediately Accessing Emergency Procedures
From any page on the MFD, press the CHKLIST Softkey.
2)
Press the EMERGCY Softkey.
3)
Turn the FMS Knob to select the desired emergency checklist and press the
ENT Key.
4)
Press the ENT Key or press the CHECK Softkey to check the selected
emergency checklist item. The line item turns green and a checkmark is
placed in the box next to it. The next line item is automatically highlighted
for checking.
EIS
1)
8)
Press the RETURN Softkey to return to the previous checklist.
9)
Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
Abnormal
Operation
Press the ENT Key to advance to the next checklist.
Additional
Features
7)
Hazard
Avoidance
Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the
cursor.
Procedures
6)
Flight
Planning
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window. If all
items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’
will be displayed in yellow text.\
GPS Nav
5)
AFCS
Press the CLR Key or press the UNCHECK Softkey to remove a check mark
from an item.
Nav/Com/
XPDR/Audio
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Annun/
Alerts
Appendix
AUXILIARY VIDEO
The G1000 system provides a control and display interface to an auxiliary video
system. The system can display video for up to two inputs.
There are four modes of operation of the auxiliary video display: Full-Screen,
Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with Map and
Digital Zoom.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
75
Additional Features
EIS
Flight
Instruments
Display Auxiliary Video
1)
Turn the large FMS Knob to select the AUX page group.
2)
Turn the small FMS Knob to select VIDEO and display the AUX-VIDEO Page.
1)
While viewing the AUX - VIDEO Page press the MENU Key to display the
Page Menu OPTIONS.
2)
Turn the large FMS Knob to highlight the desired video adjustment option
and press the ENT Key.
AFCS
Nav/Com/
XPDR/Audio
Selecting Video Menu Options
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Adjusting Video Settings
With the AUX-VIDEO Page displayed, press the SETUP Softkey.
2)
Press the BRIGHT - or BRIGHT +, to adjust display brightness in five
percent increments from 0 to 100%.
3)
Press the CNTRST - or CNTRST +, to adjust display contrast in five
percent increments from 0 to 100%.
4)
Press the SAT - or SAT +, to adjust display saturation in five percent
increments from 0 to 100%.
5)
Press the BACK Softkey to return to the previous softkey level.
Press the RESET Softkey to return the display to the default settings.
Additional
Features
Input Selection
Abnormal
Operation
With the AUX-VIDEO Page displayed, press the INPUT Softkey to switch
between Input 1 and Input 2.
Display Selection
Annun/
Alerts
With the AUX-VIDEO Page displayed, press the HIDE MAP Softkey to
switch between Split-Screen and Full Display.
Zoom/Range
Appendix
Index
1)
1)
Press the VID ZM + or VID ZM - Softkeys to increase or decrease the
video display magnification between 1x and 10x.
2)
Use the Joystick to adjust the current displayed portion of the full display.
The Joystick can be used to increase or decrease the range setting on the map
display or zoom in and out on the video display. While in the Split-Screen mode,
76
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Additional Features
Flight
Instruments
pressing the MAP ACTV or VID ACTV Softkey determines which display the Joystick
adjusts. Pressing the softkey to display MAP ACTV allows the Joystick to control the
range setting of the map display. Pressing the softkey to display VID ACTV allows the
Joystick to control the zoom setting of the video display.
EIS
ELECTRONIC STABILITY & PROTECTION (ESP™)
GPS Nav
Flight
Planning
Procedures
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
6)
Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7)
Press the FMS Knob to remove the cursor.
Abnormal
Operation
2)
Additional
Features
Turn the large FMS Knob to select the AUX Page Group.
Hazard
Avoidance
1)
Annun/
Alerts
ESP is automatically enabled on system power up.
77
Index
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the on-side
Roll Limit Indicator will move to 30°.
Appendix
Roll Engagement
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
AFCS
To Enable or Disable ESP
190-00645-08 Rev. A
Nav/Com/
XPDR/Audio
Electronic Stability and Protection (ESP™) is an optional feature that is intended
to discourage the exceedance of attitude and established airspeed parameters. This
feature will only function when the aircraft is above 200 feet AGL and the autopilot is
not engaged.
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, low
airspeed, and/or Vmo) beyond the normal flight parameters. Enhanced stability for each
condition is provided by applying a force to the appropriate control surface to return
the aircraft to the normal flight envelope. This is perceived by the pilot as resistance
to control movement in the undesired direction when the aircraft approaches a steep
attitude or high airspeed.
ESP can be enabled or disabled on the AUX-SYSTEM SETUP 2 Page on the MFD.
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Additional Features
Pitch Engagement
ESP engages at 21° nose-up and 21° nose-down. Once ESP is engaged, it will apply
opposing force between 19° and 50° nose-up and between 19° and 50° nose-down.
Maximum opposing force is applied between 25° and 50° nose-up and between 25°
and 50° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP engage and disengage limits in
these nose-up/nose-down conditions.
Decreasing airspeed to the point of an impending stall will result in ESP applying
force to lower the nose of the aircraft. In addition the ESP applied force, an
‘UNDERSPEED PROTECT ACTIVE’ warning alert is displayed. When the underspeed
condition is remedied, ESP force is no longer applied.
High Airspeed Protection
Exceeding Vmo will result in ESP applying force to raise the nose of the aircraft.
When the high airspeed condition is remedied, ESP force is no longer applied.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Underspeed Protection
78
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Additional
Features
Abnormal
Operation
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Hazard
Avoidance
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Procedures
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 failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.
Flight
Planning
ABNORMAL COM OPERATION
GPS Nav
NOTE: The Quest KODIAK 100 Pilot’s Operating Handbook (POH) always
takes precedence over the information found in this section.
AFCS
• PFD1 – By pressing the DISPLAY BACKUP button on the left audio panel.
• MFD – By pressing the DISPLAY BACKUP button on the left or the right
audio panel.
• PFD2 – By pressing the DISPLAY BACKUP button on the right audio
panel.
Nav/Com/
XPDR/Audio
Reversionary display mode can be manually activated by the pilot.
EIS
In reversionary mode, critical flight instrumentation is combined with engine
instrumentation on the remaining display.
Annun/
Alerts
Appendix
Loss of Hazard Functions with Loss of GPS
Position
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
79
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight Director
Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Extreme Pitch Indication
DEAD RECKONING
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
80
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Abnormal Operation
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. Also, the CDI deviation bar is removed from the display. Lastly, but at the same
time, a ‘GPS NAV LOST’ alert message appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different from the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compound the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Flight
Instruments
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000 stops
navigating in GPS Mode.
Annun/
Alerts
Appendix
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
Index
Dead Reckoning Indications
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
81
As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as yellow text on the display to denote degraded
navigation source information. This data includes the following:
• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
Also, while the G1000 is in DR Mode, the autopilot will not couple to GPS, and
TAWS is disabled. Additionally, the accuracy of all nearest information (airports,
airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function,
but with degraded accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
82
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
EIS
AIRCRAFT ALERTS
See the POH for information regarding pilot responses.
Annunciation Window
GPS Nav
Flight
Planning
Procedures
Repeating
Chime
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
AFCS config error. Config service req’d.
Cargo door is not closed and locked (in air).
Chip has been detected in prop gearbox.
Maximum flap speed has been exceeded.
Both fuel selectors are off.
Engine inlet in normal position. Select bypass.
Engine inlet failed to reach bypass position.
ITT red line has been exceeded.
NG red line has been exceeded.
NP red line has been exceeded.
Engine oil pressure is low.
Maximum airspeed exceeded.
UNDERSPEED PROTECT ACTIVE Fuel starvation imminent.
STALL WARNING TKS fluid quantity low. Less than 1.5 gallons.
Low TKS flow rate.
Low TKS fluid pressure.
Engine torque red line has been exceeded.
Audio
Alert
AFCS
AFCS CONFIG
CARGO DOOR
CHIP DETECTOR
FLAP OVERSPEED
FUEL OFF L-R
INLET NOT BP
INLET NOT BP
ITT
NG OVERSPEED
NP OVERSPEED
OIL PRESS LOW
OVERSPD WARN
UNDERSPEED
PROTECT ACTIVE
RESERVOIR FUEL
STALL WARNING
TKS LOW QTY
TKS LOW FLOW
TKS LOW PRESS
TORQUE
Alerts Window Message
Nav/Com/
XPDR/Audio
WARNING Alerts
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
83
CAUTION Alerts
Annunciation Window
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
ALTERNATR FL
Alternator is inoperative.
CARGO DOOR
Cargo door is not closed and locked (on ground).
EMER PWR LVR
Emergency power lever is active.
FLAP FAIL
Flight
Planning
GPS Nav
AFCS
FLAP TRIM FAIL
FUEL LOW R
Right fuel tank quantity is low.
FUEL LOW L-R
Fuel quantity is low.
FUEL PRESS LOW
Fuel pressure is low.
Procedures
INLET SW FAULT
Engine inlet position switch fault.
Hazard
Avoidance
Additional
Features
PTCH INHIB FAIL
Abnormal
Operation
PITOT FL R
Ice protection airspeed low.
Left pitot heater is inoperative.
Single
Chime
TRIM GND INHIBIT FAIL.
Right pitot heater is inoperative.
PITOT FL L-R
Both pitot heaters are inoperative.
PITOT OFF L
Left pitot heater is off.
PITOT OFF R
Right pitot heater is off.
PITOT OFF L-R
Annun/
Alerts
Ice protection airspeed high.
Engine inlet failed to reach normal position.
PITOT FL L
Appendix
Generator is inoperative.
INLET NOT NRM
LO ICE SPEED
Index
Flap Trim Failure.
Left fuel tank quantity is low.
HI ICE SPEED
Audio
Alert
Flaps system is inoperative.
FUEL LOW L
GEN FAIL
84
Alerts Window Message
Both pitot heaters are off.
STALL HT FL
Stall/AOA vane heater failure.
TKS BACKUP
Backup TKS pump selected.
TKS LOW QTY
TKS fluid quantity low. Less than 23 minutes.
TKS HI FLOW
High TKS flow rate.
TKS HI PRESS
High TKS fluid pressure.
VOLTAGE LOW
Bus voltage is below 24.0V.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Annunciation Window
AUX PUMP ON
Alerts Window Message
Flight
Instruments
Annunciation Advisory
Audio
Alert
EIS
Auxiliary fuel pump is on.
Propeller system is operating in beta mode.
CVDR RECORDING
Cockpit Voice Data Recorder is recording.
ENG INLET BP
Nav/Com/
XPDR/Audio
BETA
Engine inlet in bypass position.
FAULT CVDR
Cockpit Voice Data Recorder fault.
FUEL OFF L
Left fuel selector is off.
FUEL OFF R
Right fuel selector is off.
IGNITION ON
Engine ignition is active.
None
Cockpit Voice Data Recorder is not recording.
Engine starter is active.
TKS HI MODE
TKS high mode selected.
TKS MAX MODE
TKS max mode selected.
TKS NRM MODE
TKS normal mode selected.
AIR COND INH
Air conditioning inhibited due to insufficient Ng.
Procedures
STARTER ON
Flight
Planning
NOT RECORDING CVDR
GPS Nav
Ground Inhibit Override.
AFCS
FLAP TRIM TEST
Hazard
Avoidance
Alerts Window Message
None
Aural Alert
Description
The aircraft has descended below the preset barometric minimum
descent altitude.
“Vertical track”
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
Played when a Traffic Advisory (TA) is issued with the TIS system
or the optional GTS 800 TAS system. See the Hazard Avoidance
section for additional details on GTS 800 voice alerts..
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
85
Index
190-00645-08 Rev. A
Appendix
“Minimums, minimums”
“Traffic”
Annun/
Alerts
AURAL ALERTS
Abnormal
Operation
AVN FAN 1 FAIL – Avionics cooling fan #1 is inoperative.
AVN FAN 2 FAIL – Avionics cooling fan #2 is inoperative.
Audio Alert
None
Additional
Features
Message Advisory Alerts
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
“Traffic, Traffic”
Played when a Traffic Advisory (TA) is issued with the optional
SKY 497 TAS system. See the Skywatch PG for additional details
on voice alerts.
“TIS not available”
The aircraft is outside the Traffic Information Service (TIS) coverage
area.
“Traffic Advisory System Test
Passed”
“TAS System Test Passed”
Played when the optional traffic system passes a pilot-initiated
self test.
- SKY 497 TAS
- GTS 800 TAS
“Traffic Advisory System Test
Failed”
“TAS System Failed”
Played when the optional traffic system fails a pilot-initiated self
test.
- SKY 497 TAS
- GTS 800 TAS
Flight
Planning
“High”, “Low”, “Same
Altitude” (if within 200 feet of
own altitude), or “Altitude not
available”
Procedures
Hazard
Avoidance
Description
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
Intruder bearing (GTS 800 only).
Intruder relative altitude (GTS 800 only).
“Less than one mile”,
Intruder distance (GTS 800 only).
“One Mile” through “Ten Miles”,
or “More than ten miles”
COMPARATOR ANNUNCIATIONS
Comparator
Window Text
Abnormal
Operation
Additional
Features
Aural Alert
Condition
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
Index
Appendix
Annun/
Alerts
ALT MISCOMP Difference in altitude sensors is > 200 ft.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10
kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7
kts.
HDG MISCOMP Difference in heading sensors is > 6 degrees.
PIT MISCOMP
86
Difference in pitch sensors is > 5 degrees.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Condition
Flight
Instruments
Comparator
Window Text
ROL MISCOMP Difference in roll sensors is > 6 degrees.
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
EIS
ALT NO COMP
PIT NO COMP
Nav/Com/
XPDR/Audio
HDG NO COMP No data from one or both heading sensors.
No data from one or both pitch sensors.
ROL NO COMP No data from one or both roll sensors..
AFCS
REVERSIONARY SENSOR ANNUNCIATIONS
Condition
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading
Reference System.
BOTH ON GPS1
BOTH ON GPS2
USING ADC1
USING ADC2
USING AHRS1
USING AHRS2
USING GPS1
USING GPS2
Both PFDs are displaying data from the number one GPS receiver.
Flight
Planning
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
GPS Nav
Reversionary
Sensor Window
Text
Both PFDs are displaying data from the number two Air Data Computer.
Procedures
Both PFDs are displaying data from the number one Attitude & Heading
Reference System.
Hazard
Avoidance
Both PFDs are displaying data from the number two GPS receiver.
Additional
Features
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
Abnormal
Operation
PFD2 is displaying data from the #1 AHRS.
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
Annun/
Alerts
PFD1 is displaying data from the #2 GPS.
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
87
AFCS ALERTS
The following alert annunciations appear in the AFCS System Status field on the PFD.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Condition
Annunciation
Pitch Failure
PTCH
ROLL
YAW
Roll Failure
Flight
Planning
GPS Nav
AFCS
Yaw Damper Failure
Pitch Trim Failure
(or stuck MEPT Switch)
PTRM
System Failure
AFCS
Elevator Mistrim Down
Procedures
Aileron Mistrim Right
Hazard
Avoidance
Elevator Mistrim Up
Rudder Mistrim Right
Aileron Mistrim Left
Additional
Features
Rudder Mistrim Left
Abnormal
Operation
Preflight Test
↓ELE
↑ELE
AIL→
←AIL
RUD→
←RUD
PFT
PFT
Description
Pitch axis control failure. AP is inoperative.
Roll axis control failure. AP is inoperative.
YD control failure; AP is inoperative
If AP engaged, take control of the aircraft and
disengage AP
If AP disengaged, move MEPT switches
separately to unstick
AP and MEPT are unavailable. FD may still be
available.
Pitch servo providing sustained force in the
indicated direction. May indicate a failure of the
pitch trim servo or trim system.
Roll servo providing sustained force in the
indicated direction
Yaw servo providing sustained force in the
indicated direction. Aircraft rudder retrim after
substantial pitch and power changes required.
Performing preflight system test; aural alert
sounds at completion
Preflight system test failed; aural alert sounds at
failure
Index
Appendix
Annun/
Alerts
NOTE: Do not press the AP/YD DISC TRIM INTRPT switch during servo
power-up and preflight system tests as this may cause the preflight system
test to fail or never to start (if servos fail their power-up tests). Power must
be cycled to the servos to remedy the situation.
88
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Alert Type
MFD
Pop-Up Alert
Aural Message
EIS
PFD/MFD
TAWS-B Page
Annunciation
Flight
Instruments
TAWS-B ALERTS
“Terrain, Terrain; Pull Up, Pull
Up”
Reduced Required
Obstacle Clearance
Warning (ROC)
“Obstacle, Obstacle; Pull Up,
Pull Up”
Imminent Obstacle
Impact Warning
(IOI)
“Obstacle, Obstacle; Pull Up,
Pull Up”
Reduced Required
Terrain Clearance
Caution (RTC)
“Caution, Terrain; Caution,
Terrain”
Imminent Terrain
Impact Caution (ITI)
“Caution, Terrain; Caution,
Terrain”
Reduced Required
Obstacle Clearance
Caution (ROC)
“Caution, Obstacle; Caution,
Obstacle”
Imminent Obstacle
Impact Caution (IOI)
“Caution, Obstacle; Caution,
Obstacle”
Premature Descent
Alert Caution (PDA)
“Too Low, Terrain”
“Sink Rate”
Negative Climb
Rate Caution (NCR)
“Don’t Sink”
Appendix
Excessive Descent
Rate Caution (EDR)
Annun/
Alerts
“Five-Hundred”
Abnormal
Operation
None
Additional
Features
None
Hazard
Avoidance
Altitude Callout
“500”
Procedures
Imminent Terrain
Impact Warning (ITI)
Flight
Planning
“Terrain, Terrain; Pull Up, Pull
Up”
GPS Nav
Reduced Required
Terrain Clearance
Warning (RTC)
AFCS
“Pull Up”
Nav/Com/
XPDR/Audio
Excessive Descent
Rate Warning (EDR)
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
89
Flight
Instruments
Annunciations & Alerts
TAWS-B SYSTEM STATUS ANNUNCIATIONS
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Alert Type
PFD/MFD Alert
Annunciation
System Test in Progress
System Test Pass
None
TAWS-B FLTA Alerting
Inhibited
MFD Terrain or Obstacle
database unavailable
or invalid, TAWS-B
operating with PFD
Terrain or Obstacle
databases
None
TAWS-B System Test
Fail; Terrain or Obstacle
database unavailable or
invalid; Invalid software
configuration; or System
audio fault
No GPS position
Excessively degraded
GPS signal, Out of
database coverage area
TAWS-B Page Annunciation
Aural Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
MFD & PFD MESSAGE ADVISORIES
Message
Comments
DATA LOST – Pilot stored data was The pilot profile data was lost. System reverts
lost. Recheck settings.
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
XTALK ERROR – A flight display
The MFD and PFDs are not communicating with
crosstalk error has occurred.
each other. The system should be serviced.
90
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
GPS Nav
Flight
Planning
The PFD configuration settings do not match
backup configuration memory. The system
should be serviced.
Procedures
The MFD configuration settings do not match
backup configuration memory. The system
should be serviced.
Hazard
Avoidance
Additional
Features
The specified GDU has different software
versions installed. The system should be
serviced.
Abnormal
Operation
Annun/
Alerts
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the system should
be serviced.
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Appendix
190-00645-08 Rev. A
The PFD and/or MFD self-test has detected a
problem. The system should be serviced.
EIS
PFD1 SOFTWARE – PFD1
mismatch, communication halted.
PFD2 SOFTWARE – PFD2
mismatch, communication halted.
MFD1 SOFTWARE – MFD1
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.
Comments
Flight
Instruments
Message
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD2 SERVICE – PFD2 needs
service. Return unit for repair.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
PFD1 MANIFEST – PFD1 software
mismatch, communication halted.
PFD2 MANIFEST – PFD2 software
mismatch, communication halted.
MFD1 MANIFEST – MFD1
software mismatch, communication
halted.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
PFD2 CONFIG – PFD2 config error.
Config service req’d.
MFD1 CONFIG – MFD1 config
error. Config service req’d.
91
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
PFD2 KEYSTK – PFD2 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is
inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage.
PFD2 VOLTAGE – PFD2 has low
voltage. Reducing power usage.
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage.
[PFD1, PFD2, or MFD1] BKLT CAL
INV – calibration lost or mismatch.
Return for repair.
Comments
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if
the problem persists.
The PFD1 configuration module backup memory
has failed. The system should be serviced.
The PFD1 voltage is low. The system should be
serviced.
The PFD2 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
The PFD1, PFD2 and/or MFD backlight
calibration cannot be found or is invalid. The
system should be serviced.
DATABASE MESSAGE ADVISORIES
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
PFD2 DB ERR – PFD2 navigation
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.
92
Comments
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
navigation database. If problem persists, the
system should be serviced.
The MFD and/or PFD detected a failure in the
basemap database. The G1000 system should be
serviced.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Comments
Flight
Instruments
The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card
is properly inserted in display. Replace terrain
card. If problem persists, the system should be
serviced.
EIS
Nav/Com/
XPDR/Audio
AFCS
The terrain database is present on another LRU,
but is missing on the specified LRU.
GPS Nav
Additional
Features
Abnormal
Operation
Annun/
Alerts
The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the G1000 system should be
serviced.
Hazard
Avoidance
The obstacle database is present on another
LRU, but is missing on the specified LRU. Ensure
that the terrain card is properly inserted in
the specified display. Replace terrain card. If
problem persists, the G1000 system should be
serviced.
Procedures
The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the G1000 system should be serviced.
Flight
Planning
Appendix
Message
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
PFD2 DB ERR – PFD2 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
PFD2 DB ERR – PFD2 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
PFD2 DB ERR – PFD2 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD2 DB ERR – PFD2 obstacle
database missing.
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
PFD2 DB ERR – PFD2 airport
terrain database error exists.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
93
Message
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
PFD2 DB ERR – PFD2 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD2 DB ERR – PFD2 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Comments
The MFD and/or PFD detected a failure in the
airport terrain database. Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the G1000 system should be
serviced.
The MFD and/or PFD detected a failure in the
Safe Taxi database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
The MFD and/or PFD detected a failure in the
ChartView database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, the system should
be serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD and/or PFDs detected a failure in the
database error exists.
FliteCharts database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, the system should
be serviced.
MFD1 DB ERR – MFD1 Airport
The MFD detected a failure in the Airport
Directory database error exists.
Directory database. Ensure the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
94
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
The PFDs and MFD have different navigation
database versions or regions installed. Crossfill
is off. Check the AUX-SYSTEM STATUS Page
to determine versions or regions. Also, check
the AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Standby
The PFDs and MFD have different standby
Navigation database mismatch.
navigation database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to
determine versions or regions. Also, check the
AUX-SYSTEM STATUS Page for a database
synchronization function not completed. After
synchronization is complete, power must be
turned off, then on.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database mismatch.
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
Flight
Instruments
Message
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
95
Message
DB MISMATCH – Airport Terrain
database mismatch.
NAV DB UPDATED – Active
navigation database updated.
TERRAIN DSP – [PFD1, PFD2 or
MFD1] Terrain awareness display
unavailable.
Comments
The PFDs and MFD have different airport terrain
database versions or regions installed. Check
the AUX-SYSTEM STATUS Page to determine
versions or regions. Also, check the AUX-SYSTEM
STATUS Page for a database synchronization
function not completed. After synchronization is
complete, power must be turned off, then on.
System has updated the active navigation
database from the standby navigation database.
One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD
or MFD is missing or invalid.
GMA 1347 MESSAGE ADVISORIES
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
GMA2 FAIL – GMA2 is inoperative. The audio panel is unavailable. The G1000
system should be serviced.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data between
has occurred.
the two GMAs. The G1000 system should be
serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The
GMA2 CONFIG – GMA2 config
G1000 system should be serviced.
error. Config service req’d.
GMA 1 MANIFEST –
GMA1 software mismatch.
Communication halted.
The audio panel has incorrect software installed.
The G1000 system should be serviced.
GMA 2 MANIFEST – GMA2
software mismatch, communication
halted.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
96
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
Hazard
Avoidance
Abnormal
Operation
Annun/
Alerts
The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.
Additional
Features
The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.
Index
97
Appendix
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Procedures
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Flight
Planning
The GIA1 and/or GIA2 have an error in the audio
configuration. The G1000 system should be
serviced.
GPS Nav
190-00645-08 Rev. A
Comments
AFCS
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
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.
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Nav/Com/
XPDR/Audio
GIA 63W MESSAGE ADVISORIES
EIS
Comments
The 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.
Flight
Instruments
Message
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
GMA2 SERVICE – GMA2 needs
service. Return unit for repair.
Message
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
GIA1 MANIFEST – GIA1 software
mismatch, communication halted.
GIA2 MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software
mismatch, communication halted.
COM1 MANIFEST– COM1
software mismatch, communication
halted.
COM2 MANIFEST– COM2
software mismatch, communication
halted.
NAV1 MANIFEST– NAV1 software
mismatch, communication halted.
NAV2 MANIFEST– NAV2 software
mismatch, communication halted.
COM1 CONFIG – COM1 config
error. Config service req’d.
COM2 CONFIG– COM2 config
error. Config service req’d.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
Comments
A GIA mismatch has been detected, where only
one is SBAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
COM1 and/or COM2 software mismatch. The
G1000 system should be serviced.
NAV1 and/or NAV2 software mismatch. The
G1000 system should be serviced.
COM1 and/or COM2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
The system has detected an over-temperature
condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If the
problem persists, the system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
98
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Comments
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
99
GPS Nav
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
AFCS
190-00645-08 Rev. A
Nav/Com/
XPDR/Audio
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 system should be
serviced.
COM1 RMT XFR – COM1 remote The COM1 and/or COM2 transfer switch is stuck
transfer key is stuck.
in the enabled (or “pressed”) position. Press
COM2 RMT XFR – COM2 remote the transfer switch again to cycle its operation.
If the problem persists, the system should be
transfer key is stuck.
serviced.
LOI – GPS integrity lost. Crosscheck GPS integrity is insufficient for the current phase
with other NAVS.
of flight.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to insufficient
navigation. Insufficient satellites.
satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
ABORT APR – Loss of GPS
Abort approach due to loss of GPS navigation.
navigation. Abort approach.
APR DWNGRADE – Approach
Vertical guidance generated by SBAS is
downgraded.
unavailable, use LNAV only minimums.
TRUE APR – True north approach. Displayed after passing the first waypoint of a true
Change HDG reference to TRUE.
north approach when the nav angle is set to ‘AUTO’.
GPS1 SERVICE – GPS1 needs
A failure has been detected in the GPS1 and/
service. Return unit for repair.
or GPS2 receiver. The receiver may still be
GPS2 SERVICE – GPS2 needs
available. The system should be serviced.
service. Return unit for repair.
EIS
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.
Flight
Instruments
Message
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk
key is stuck.
COM2 PTT – COM2 push-to-talk
key is stuck.
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be
available. The system should be serviced.
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, the system should be
serviced.
G/S2 FAIL – G/S2 is inoperative.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The system should
be serviced.
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
GEA 71 MESSAGE ADVISORIES
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
G1000 system should be serviced.
GEA1 MANIFEST – GEA1 software The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GEA2 MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed.
mismatch, communication halted. The G1000 system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
G/S1 FAIL – G/S1 is inoperative.
Comments
100
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Comments
The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.
EIS
Nav/Com/
XPDR/Audio
The transponder has incorrect software installed.
The system should be serviced.
GPS Nav
The #1 transponder should be serviced when
possible.
The #2 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
There is no communication with the #2
transponder.
Flight
Planning
Procedures
Appendix
Index
101
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Abnormal
Operation
190-00645-08 Rev. A
Additional
Features
AHRS2 TAS – AHRS2 not receiving
valid airspeed.
Comments
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 system should be serviced.
The #2 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The system should be serviced.
Hazard
Avoidance
ADS-B is inoperative. The transponder may
not be receiving a valid GPS position. Other
transponder functions may be available. Service
when possible.
GRS 77 MESSAGE ADVISORIES
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
AFCS
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
XPDR2 CONFIG – XPDR2 config
error. Config service req’d.
GTX1 MANIFEST – GTX1 software
mismatch, communication halted.
GTX2 MANIFEST – GTX2 software
mismatch, communication halted.
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR2 SRVC – XPDR2 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is
inoperative.
XPDR2 FAIL – XPDR2 is
inoperative.
XPDR1 ADS-B FAIL – XPDR1 is
unable to transmit ADS-B messages.
XPDR2 ADS-B FAIL – XPDR2 is
unable to transmit ADS-B messages.
Flight
Instruments
GTX 33 MESSAGE ADVISORIES
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
Comments
AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path.
GPS source.
Primary GPS path has failed. The system should
be serviced when possible.
AHRS2 GPS – AHRS2 using backup The #2 AHRS is using the backup GPS path.
GPS source.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful
any GPS information.
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving any or any useful
any GPS information.
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be serviced.
AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be serviced.
AHRS1 GPS – AHRS1 operating
The #1 AHRS is operating exclusively in no-GPS
exclusively in no-GPS mode.
mode. The system should be serviced.
AHRS2 GPS – AHRS2 operating
The #2 AHRS is operating exclusively in no-GPS
exclusively in no-GPS mode.
mode. The system should be serviced.
AHRS MAG DB – AHRS magnetic
The #1 AHRS and #2 AHRS magnetic model
model database version mismatch. database versions do not match.
AHRS1 SRVC – AHRS1 Magnetic- The #1 AHRS earth magnetic field model is out of
field model needs update.
date. Update magnetic field model when practical.
AHRS2 SRVC – AHRS2 Magnetic- The #2 AHRS earth magnetic field model is out of
field model needs update.
date. Update magnetic field model when practical.
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass. The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged
GEO LIMITS – AHRS2 too far
as invalid.
North/South, no magnetic compass.
GRS1 MANIFEST – GRS1 software The #1 AHRS has incorrect software installed.
mismatch, communication halted.
The G1000 system should be serviced.
102
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
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Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Procedures
Comments
A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.
A fault has occurred in the #2 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000
system should be serviced.
GMU1 MANIFEST – GMU1
software mismatch, communication
halted.
The GMU 44 has incorrect software installed.
The G1000 system should be serviced.
GMU 2 MANIFEST – GMU2
software mismatch, communication
halted.
190-00645-08 Rev. A
Flight
Planning
HDG FAULT – AHRS2
magnetometer fault has occurred.
GPS Nav
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
AFCS
GMU 44 MESSAGE ADVISORIES
Nav/Com/
XPDR/Audio
AHRS1 CAL – AHRS1 calibration
version error. Srvc req’d.
AHRS2 CAL – AHRS2 calibration
version error. Srvc req’d.
EIS
AHRS2 CONFIG – AHRS2 config
error. Config service req’d.
Comments
The #2 AHRS has incorrect software installed.
The system should be serviced.
A failure has been detected in the #1 AHRS. The
system should be serviced.
A failure has been detected in the #2 AHRS. The
system should be serviced.
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
AHRS configuration settings do not match those
of backup configuration memory. The system
should be serviced.
The #1 AHRS calibration version error. The system
should be serviced.
The #2 AHRS calibration version error. The system
should be serviced.
Flight
Instruments
Message
GRS2 MANIFEST – GRS2 software
mismatch, communication halted.
AHRS1 SERVICE – AHRS1 needs
service. Return unit for repair.
AHRS2 SERVICE – AHRS2 needs
service. Return unit for repair.
AHRS1 CONFIG – AHRS1 config
error. Config service req’d.
103
GWX 68 MESSAGE ADVISORIES
Message
GWX CONFIG – GWX config error.
Config service req’d.
GWX FAIL – GWX is inoperative.
GWX SERVICE – GWX needs
service. Return unit for repair.
GWX MANIFEST – GWX software
mismatch, communication halted.
WX ALERT – Possible severe
weather ahead.
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.
The GDU is not receiving status packet from the
GWX 68 or the GWX 68 is reporting a fault.
The GWX 68 radar system should be serviced.
A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
The GWX 68 has incorrect software installed.
The system should be serviced.
Possible severe weather detected within +/- 10
degrees of the aircraft heading at a range of 80
to 320 nm.
GDL 69A/69A SXM MESSAGE ADVISORIES
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL69 FAIL – GDL 69 has failed.
GDL69 MANIFEST – GDL software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GDL 69. The
receiver is unavailable. The system should be
serviced
The GDL 69 has incorrect software installed.
The G1000 system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
104
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Comments
GDC1 or GDC2 is reporting that the altitude
error correction is unavailable. The G1000
system should be serviced.
EIS
Nav/Com/
XPDR/Audio
GDC1 or GDC2 is reporting that the airspeed
error correction is unavailable. The G1000
system should be serviced.
AFCS
GPS Nav
The GDC1 should be serviced.
The GDC2 should be serviced.
Flight
Planning
The GDC1 or GDC2 has incorrect software
installed. The system should be serviced.
Procedures
Message
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC2 ALT EC – ADC2 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC2 AS EC – ADC2 airspeed error
correction is unavailable.
ADC1 SERVICE – ADC1 needs
service. Return unit for repair.
ADC2 SERVICE – ADC2 needs
service. Return unit for repair.
GDC1 MANIFEST – GDC1 software
mismatch, communication halted.
GDC2 MANIFEST – GDC2 software
mismatch, communication halted.
Flight
Instruments
GDC 74A MESSAGE ADVISORIES
Hazard
Avoidance
GMC 710 MESSAGE ADVISORIES
Comments
Additional
Features
Error in the configuration of the GMC 710.
105
Index
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Appendix
190-00645-08 Rev. A
Annun/
Alerts
A failure has been detected in the GMC 710.
The GMC 710 is unavailable.
GMC MANIFEST – GMC software The GMC 710 has incorrect software installed.
mismatch, communication halted.
The G1000 system should be serviced.
GMC KEYSTK – GMC [keyname]
A key is stuck on the GMC 710 bezel. Attempt
Key is stuck
to free the stuck key by pressing it several times.
The G1000 system should be serviced if the
problem persists.
SPD KEY DISABLED - The SPD key The SPD Key on GMC 710 has no function in
is disabled for this model aircraft.
this aircraft model.
Abnormal
Operation
Message
GMC CNFG – GMC Config error.
Config service req’d.
GMC FAIL – GMC is inoperative.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GTS 800 MESSAGE ADVISORIES
Message
GTS CONFIG – GTS config error.
Config service req’d.
GTS MANIFEST – GTS software
mismatch, communication halted.
Comments
The GTS and GDU have different copies of the
GTS configuration, or the Mode S address is
invalid. The G1000 system should be serviced.
The GTS has incorrect software installed. The
G1000 system should be serviced.
MISCELLANEOUS MESSAGE ADVISORIES
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Comments
Upon power-up, the G1000 system detects that
a stored flight plan waypoint is locked. This
occurs when an navigation database update
eliminates an obsolete waypoint. The flight
plan cannot find the specified waypoint and
flags this message. This can also occur with
user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it
no longer exists in any database,
Or - update the waypoint name/identifier to
reflect the new information.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint
waypoint moved.
coordinate has changed due to a new
navigation database update. Verify that stored
flight plans contain correct waypoint locations.
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
DB CHANGE – Database changed. This occurs when a stored flight plan contains a
Verify user modified procedures.
procedure that is no longer consistent with the
navigation database. This alert is issued only
after a navigation database update. Verify that
the user-modified procedures in stored flight
plans are correct and up to date.
106
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
This occurs when a stored flight plan contains
an airway that is no longer consistent with the
navigation database. This alert is issued only
after a navigation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
FPL TRUNC – Flight plan has been This occurs when a newly installed navigation
truncated.
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate
locked flight plan.
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint -[xxxx]
waypoint name.
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to
turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the special use airspace.
ARSPC AHEAD – Airspace ahead
Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the special use airspace
within 10 minutes.
ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
APPR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
Flight
Instruments
Message
DB CHANGE – Database changed.
Verify stored airways.
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
107
Message
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on CDI for
approach.
PTK FAIL – Parallel track
unavailable: bad geometry.
PTK FAIL – Parallel track
unavailable: invalid leg type.
PTK FAIL – Parallel track
unavailable: past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
VNV – Unavailable. Unsupported
leg type in flight plan.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Do not use GPS
for navigating to -[xxxx]
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
108
Comments
The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
The system notifies the pilot to set the CDI to
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been
passed.
The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.
The lateral flight plan contains a procedure
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
A parallel course has been selected, causing the
vertical deviation to go invalid.
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to
the selected non-WGS84 waypoint.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
109
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Procedures
190-00645-08 Rev. A
Flight
Planning
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
[PFD1, PFD2, or MFD1] CARD
1 REM – Card 1 was removed.
Reinsert card.
[PFD1, PFD2, or MFD1] CARD
2 REM – Card 2 was removed.
Reinsert card.
GPS Nav
USER MAG VAR – User magnetic
variation is active.
AFCS
SVT DISABLED – Terrain DB
resolution too low.
Nav/Com/
XPDR/Audio
SCHEDULER [#] – <message>.
SVT DISABLED – Out of available
terrain region.
EIS
STRMSCP FAIL – Stormscope has
failed.
FAILED PATH – A data path has
failed.
MAG VAR – Large magnetic
variance. Verify all course angles.
Comments
The system is no longer receiving data from
the traffic system. The traffic device should be
serviced.
Stormscope has failed. The G1000 system
should be serviced.
A data path connected to the GDU or the GIA
63/W has failed.
The GDU’s internal model cannot determine
the exact magnetic variance for geographic
locations near the magnetic poles. Displayed
magnetic course angles may differ from the
actual magnetic heading by more than 2°.
Message criteria entered by the user.
Synthetic Vision is disabled because the aircraft
is not within the boundaries of the installed
terrain database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second
or better) is not currently installed.
User magnetic variation mode was selected
during previous operation and is still active
(checked at power-up.)
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
The SD card was removed from the top card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
The SD card was removed from the bottom card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
Flight
Instruments
Message
TRAFFIC FAIL – Traffic device has
failed.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Message
[PFD1, PFD2, or MFD1] CARD 1
ERR – Card 1 is invalid.
[PFD1, PFD2, or MFD1] CARD 2
ERR – Card 2 is invalid.
TRN AUD FAIL – Trn Awareness
audio source unavailable.
TERRAIN AUD CFG – Trn Awareness
audio config error. Service req’d.
TERRAIN DISABLED – Terrain
Awareness DB resolution too low.
Comments
The SD card in the top card slot of the specified
PFD or MFD contains invalid data.
The SD card in the bottom card slot of the
specified PFD or MFD contains invalid data.
The audio source for terrain awareness is
offline. Check GIA1 or GIA 2.
Terrain audio alerts are not configured properly.
The system should be serviced
TAWS is disabled because a terrain database of
sufficient resolution (9 arc-second or better) is
not currently installed.
HOLD EXPIRED – Holding EFC time Expect Further Clearance (EFC) time has expired
expired.
for the User Defined Hold.
BARO MISMATCH – Correct baro
Altimeter setting is not the same on PFD1 and
mismatch for VNAV guidance.
PFD2. Synchronize settings for VNAV guidance.
ESP OFF – ESP selected off.
Electronic Stability and Protection has been
disabled on the AUX-SYSTEM SETUP 2 page.
ESP FAIL – ESP is inoperative.
The ESP function has failed and is inoperative.
The system should be serviced.
ESP DEGRADE – ESP IAS mode is
IAS mode of ESP is inoperative. The system
inoperative.
should be serviced.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
Description
‘Flight plan successfully imported.’ A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints
The file stored on the SD card did not contain a flight
only. User waypoints imported
plan, only user waypoints. These waypoints have been
successfully. No stored flight plan saved to the system user waypoints. No flight plans
data was modified.’
stored in the system have been modified.
110
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Annunciations & Alerts
The SD card contains no flight plan data.
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Flight plan data was not successfully imported from the
SD card.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported
from the SD card; however others had errors and were
not imported. A partial stored flight plan now exists in
the system.
‘File contained user waypoints
The file stored on the SD card did not contain a flight
only.’
plan, only user waypoints. One or more of these
waypoints did not import successfully.
‘Too many points. Flight plan
The flight plan on the SD card contains more waypoints
truncated.’
than the system can support. The flight plan was
imported with as many waypoints as possible.
‘Some waypoints not loaded.
The flight plan on the SD card contains one or
Waypoints locked.’
more waypoints that the system cannot find in
the navigation database. The flight plan has been
imported, but must be edited within the system before
it can be activated for use.
‘User waypoint database full. Not The flight plan file on the SD card contains user
all loaded.’
waypoints. The quantity of stored user waypoints has
exceeded system capacity; therefore, not all the user
waypoints on the SD card have been imported. Any
flight plan user waypoints that were not imported are
locked in the flight plan. The flight plan must be edited
within the system before it can be activated for use.
‘One or more user waypoints
One or more imported user waypoints were renamed
renamed.’
when imported due to naming conflicts with waypoints
already existing in the system.
‘Flight plan successfully exported.’ The stored flight plan was successfully exported to the
SD card.
EIS
‘No flight plan files found to
import.’
‘Flight plan import failed.’
Description
Flight
Instruments
Flight Plan Import/Export
Results
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
111
Flight Plan Import/Export
Results
‘Flight plan export failed.’
Description
The stored flight plan was not successfully exported
to the SD card. The SD card may not have sufficient
available memory or the card may have been removed
prematurely.
PILOT PROFILE IMPORT/EXPORT MESSAGES
Flight Plan Import/Export
Results
Description
‘No pilot profile plan files found Displayed if the SD card does not have one or more
to import.’
valid pilot profile filenames.
‘Overwrite existing profile?’
Displayed if the profile name matches the name of
existing profile.
‘Profile name invalid. Enter a
Displayed if the profile name is invalid.
different profile name.’
‘All available pilot profiles in
Displayed if the maximum number for pilot profiles
use. Delete a profile before
has been reached.
importing another.’
‘Pilot profile import failed.’
Displayed if the importing operation fails for any
other reason.
‘Pilot profile import succeeded.’ Displayed if the importing operation succeeds.
‘Overwrite existing file?’
Displayed if the filename matches the name of an
existing file on the SD card.
‘Pilot profile export failed.’
Displayed if the export operation fails.
‘Pilot profile export succeeded.’ Displayed if the export operation succeeds.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
112
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EIS
ALERTS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Top Level PFD Softkeys
ALERTS
Flight
Planning
METAR
STRMSCP
TRFC-1
ALERTS
Additional
Features
Inset Map Softkeys
Level 2
Level 3
Description
Displays Inset Map in PFD lower left corner
INSET
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features
visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the
active flight plan
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
113
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Level 1
Hazard
Avoidance
Select the BACK Softkey to return to
the top-level softkeys.
TRFC-2
Procedures
WX LGND
Level 1
Level 2
Level 3
TRAFFIC
Nav/Com/
XPDR/Audio
AFCS
TOPO
TERRAIN
Press to display the Stormscope lightning
data on the Inset Map (within a 200 nm
radius of the aircraft)
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM WX lightning information on
Inset Map (optional feature)
Displays METAR flags on airport symbols
shown on the Inset Map (optional)
Flight
Planning
GPS Nav
STRMSCP
NEXRAD
XM LTNG
Procedures
Description
Displays icon and age on the Inset Map for
the selected weather products (optional)
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in
the inset map window
Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation
scale on Inset Map
Displays terrain information on Inset Map
WX LGND
EIS
Flight
Instruments
Appendix
Hazard
Avoidance
METAR
Additional
Features
ALERTS
ADC2
Abnormal
Operation
ADC1
BACK
AHRS2
ALERTS
Select the BACK Softkey to
return to the top level softkeys.
Annun/
Alerts
Sensor Softkeys
Level 1
Level 2
114
Level 3
Description
ADC1
Displays softkeys for selecting the #1 and
#2 AHRS and Air Data Computers
Selects the #1 Air Data Computer
ADC2
Selects the #2 Air Data Computer
SENSOR
Index
Appendix
AHRS1
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Level 2
Level 3
Description
AHRS1
Selects the #1 AHRS
AHRS2
Selects the #2 AHRS
Flight
Instruments
Level 1
EIS
ALERTS
ALERTS
ALT UNIT
HSI FMT
Nav/Com/
XPDR/Audio
SYN VIS
AFCS
Select the BACK Softkey to
return to the top-level softkeys
GPS Nav
METERS
BACK
ARC HSI
IN
HPA
ALERTS
Flight
Planning
360 HSI
ALERTS
Procedures
ALERTS
SYN TERR HRZN HDG APTSIGNS
Hazard
Avoidance
PATHWAY
ALERTS
Additional
Features
PFD Configuration Softkeys
Level 2
Level 3
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
115
Index
SYN TERR
Appendix
PATHWAY
Annun/
Alerts
SYN VIS
Description
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes
representing the horizontal and vertical
flight path of the active flight plan
Enables synthetic terrain depiction
Abnormal
Operation
Level 1
PFD
Level 1
Level 2
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
AFCS
DFLTS
Procedures
Flight
Planning
GPS Nav
WIND
Level 3
Description
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings,
including changing units to standard
Displays softkeys to select wind data
parameters
Headwind/tailwind and crosswind
OPTN 1
arrows with numeric speed components
Wind direction arrow with numeric
OPTN 2
headwind/tailwind and crosswind speeds
Wind direction arrow with numeric
OPTN 3
direction and speed
Information not displayed
OFF
Additional
Features
Hazard
Avoidance
BRG1
HSI FRMT
Abnormal
Operation
360 HSI
ARC HSI
Appendix
Annun/
Alerts
BRG2
Index
ALT UNIT
116
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree
format
Displays the HSI in an arc format
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays softkeys for setting the
altimeter and BARO settings to metric
units
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Level 2
IN
Press to display the BARO setting as
inches of mercury
HPA
Press to display the BARO setting as
hectopacals
Nav/Com/
XPDR/Audio
Description
When enabled, displays altimeter in
meters
EIS
Level 3
METERS
Flight
Instruments
Level 1
AFCS
Sets barometric pressure to 29.92 in
Hg (1013 hPa)
STD BARO
ALERTS
GPS Nav
ALERTS
Hazard
Avoidance
Press the BACK Softkey to return
to the top-level softkeys.
Transponder Softkeys
Level 2
Level 3
Description
CDI
ON
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
190-00645-08 Rev. A
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Appendix
STBY
Annun/
Alerts
XPDR
Abnormal
Operation
Selects OBS mode on the CDI when
navigating by GPS (only available with active
leg)
Cycles through GPS, VOR1, and VOR2
navigation modes on the CDI
Displays transponder mode selection softkeys
OBS
Additional
Features
Level 1
Procedures
ALERTS
Flight
Planning
Press the BACK Softkey to return
to the top-level softkeys.
117
Level 1
Level 2
Level 3
0—7
BKSP
Removes numbers entered, one at a time
IDENT
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
ALERT
Displays Alerts Window
AFCS
Nav/Com/
XPDR/Audio
GND
VFR
Procedures
Flight
Planning
GPS Nav
CODE
Hazard
Avoidance
IDENT
Additional
Features
IDENT
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Description
Selects Mode C – Altitude Reporting Mode
(transponder replies to identification and
altitude interrogations)
Manually selects Ground Mode, the
transponder does not allow Mode A
and Mode C replies, but it does permit
acquisition squitter and replies to discretely
addressed Mode S interrogations.
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
ALT
EIS
Flight
Instruments
Appendix
118
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
DCLTR
MAP
ENGINE
Press the BACK Softkey on this
level to return to the top softkey level.
SYSTEM
(optional)
(optional)
DCLTR-2
BACK
FUEL
CHKLIST
EIS
ENGINE
DCLTR-1
SHW CHRT
Flight
Instruments
MFD SOFTKEY MAP
DCLTR-3
PROFILE
TOPO
TERRAIN
Press the BACK Softkey on this
level to return to the top softkey level.
(optional)
(optional)
(optional)
(optional)
(optional)
NEXRAD
XM LTNG
METAR
LEGEND
WX RADAR
Nav/Com/
XPDR/Audio
TRAFFIC
(Default softkey
is dependant on
the selection made
in the map setup
options)
(optional)
AIRWAYS
STRMSCP
BACK
AFCS
AIRWY ON
AIRWY LO
ENGINE
SYSTEM
FUEL
DEC FUEL
INC FUEL
RST FUEL
GPS Nav
AIRWAY HI
BACK
ENGINE
DONE
EXIT
EMERGCY
Level 2
Level 3
Description
Displays the SYSTEM engine display
FUEL
Displays the fuel adjustment softkeys
Abnormal
Operation
SYSTEM
Additional
Features
ENGINE
Displays the default engine softkey
level
Displays oil, electrical, and fuel sliders
ENGINE
Hazard
Avoidance
Level 1
Procedures
MFD Softkeys
Flight
Planning
The DONE Softkey changes to UNDO when the checklist
item is already checked
Press the BACK Softkey on this
level to return to the top softkey level.
Annun/
Alerts
DEC FUEL Decreases the fuel remaining in
10-pound increments
INC FUEL Increases the fuel remaining in
10-pound increments
RST FUEL Resets the fuel remaining to 2200
pounds
Returns to previous level softkeys
BACK
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
119
Level 1
Level 2
MAP
TRAFFIC
EIS
Flight
Instruments
Appendix
Nav/Com/
XPDR/Audio
PROFILE
AFCS
TOPO
GPS Nav
TERRAIN
Hazard
Avoidance
Procedures
Flight
Planning
AIRWAYS
Additional
Features
XM LTNG
Annun/
Alerts
NEXRAD
Abnormal
Operation
STRMSCP
Appendix
METAR
Index
LEGEND
120
Level 3
Description
Enables second-level Navigation Map
softkeys
Displays traffic information on
Navigation Map
Displays/removes profile view on
Navigation Map
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Navigation Map
Displays terrain information on
Navigation Map
Displays airways on the map; cycles
through the following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways
are displayed
AIRWY HI: Only high altitude
airways are displayed
Displays Stormscope weather and
coverage information on Navigation
Map (optional feature)
Displays NEXRAD weather and
coverage information on Navigation
Map (optional feature)
Displays XM WX lightning information
on Navigation Map (optional feature)
Displays METAR flags on airport
symbols shown on the Navigation Map
(optional)
Displays the legend for the selected
weather products. Available only when
NEXRAD, XM LTNG, and/or METAR
softkeys are selected.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Level 2
WX
RADAR
Description
Displays/removes airborne weather
radar information on Navigation Map
Page
Returns to top-level softkeys
EIS
BACK
Level 3
Flight
Instruments
Level 1
Index
121
Appendix
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Annun/
Alerts
190-00645-08 Rev. A
Abnormal
Operation
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database features.
Additional
Features
NOTE: DO NOT use the database SD cards for any purpose other than database
storage.
Hazard
Avoidance
NOTE: When loading database updates, the ‘DB Mismatch’ message will
be displayed until database synchronization is complete, followed by turning
system power off, then on. Synchronization can be monitored on the AUXSYSTEM STATUS Page.
Procedures
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in
maintenance being required to reboot the system.
Flight
Planning
UPDATING DATABASES
GPS Nav
CHKLIST
AFCS
SHW CHRT
Nav/Com/
XPDR/Audio
Selects desired amount of map detail;
cycles through declutter levels:
DCLTR (No Declutter): All map
features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA
data
DCLTR-3: Removes everything except
the active flight plan
When available, displays optional
airport and terminal procedure charts
When available, displays optional
checklists
DCLTR (3)
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error message
is displayed, the problem must be corrected before synchronization can be completed.
A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown.
Error Message
Description
Canceled
Database synchronization has been canceled by removing the
bottom SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
Updating Basemap, SafeTaxi, Airport Terrain, Obstacle, and Airport
Directory Databases
These databases may be copied to one Supplemental Data Card, then automatically
synchronized to the other cards in the system:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
122
1)
With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
2)
Update the basemap, SafeTaxi, airport terrain, obstacle and/or airport
directory databases on the MFD card.
3)
Insert the MFD database card into the bottom card slot of the MFD.
4)
Apply power to the system, check that the databases are initialized and
displayed on the power-up screen. If a ‘Verifying’ message is seen, wait for
the system to finish loading before proceeding to step 5.
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right-most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
9)
Remove and reapply power to the system.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
11) Turn the small FMS Knob to select the System Status Page.
Nav/Com/
XPDR/Audio
Updating Terrain, FliteCharts, and ChartView Databases
3)
Insert the updated Supplemental Data Cards into the bottom card slot of
the MFD and PFD. The Supplemental Data Card containing the FliteCharts
or ChartView database is inserted in the MFD.
4)
Apply power to the system, check that the databases are initialized and
displayed on the power-up screen. A ‘Verifying’ message may be seen.
If this message is present, wait for the system to finish loading before
proceeding to step 5.
5)
Acknowledge the Power-up Page agreement by pressing the ENT Key or
the right-most softkey.
6)
Turn the large FMS Knob to select the AUX Page group on the MFD.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB or PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
9)
Remove power from the system.
Procedures
Copy the updated terrain database to both Supplemental Data Cards. Copy
the updated FliteCharts or ChartView database to one Supplemental Data
Card.
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Loading the Jeppesen Navigation Database as the Active Navigation
Database
123
Index
NOTE: Loading the Jeppesen Navigation Database as the active database
prior to its effective date will result in the expiration date on the power-up
screen and the effective date on the AUX-System Status Page being displayed
in yellow.
Appendix
The Jeppesen Navigation Database that is loaded to internal memory as the active
database will be used by the system.
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Flight
Planning
2)
GPS Nav
With system power OFF, remove the Supplemental Data Card from the
bottom card slot of the MFD and PFD.
AFCS
1)
190-00645-08 Rev. A
EIS
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB or PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
Flight
Instruments
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Flight
Instruments
Appendix
EIS
With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated
(label of SD card facing left).
2)
Turn the system ON. A prompt is displayed in the upper left corner of the
display:
3)
4)
Press the NO Softkey to proceed to loading the active database.
A prompt similar to the following is displayed. Press the YES Softkey to update
the active navigation database.
5)
After the update completes, the display starts in normal mode.
6)
Turn the system OFF and remove the SD card from the top card slot.
7)
Repeat steps 1 through 6 for the other displays (PFD1, PFD2, or MFD).
8)
Apply power to the system and press the ENT Key to acknowledge the startup
screen.
9)
Turn the large FMS Knob to select the AUX Page group on the MFD.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
1)
Nav/Com/
XPDR/Audio
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
10) Turn the small FMS Knob to select the System Status Page.
124
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Nav/Com/
XPDR/Audio
AFCS
The purpose of the Standby Navigation Database is to allow the loading of the
next cycle of the Jeppesen Navigation Database to the bottom SD card, prior to its
effective date. (The Jeppesen Navigation Database is available from Jeppesen seven
days prior to its effective date.)
EIS
Loading the Jeppesen Navigation Database as the Standby Navigation
Database
Flight
Instruments
11) Press the Display Database Selection Softkey to show active navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify
the correct active navigation database cycle information is shown for each
display.
With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the MFD.
2)
Verify that an SD card is inserted in the bottom slot of each PFD and the
MFD.
3)
Turn the system ON. A prompt similar to the following is displayed.
4)
Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
5)
After the navigation database files are copied to the bottom SD card, the
display will appear as shown in the following figure.
Flight
Planning
1)
GPS Nav
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
125
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
As instructed on the display, press any key to continue. The display will now
appear as shown in the following figure.
7)
Press any key to continue. The display will now appear as shown in the
following figure.
8)
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
9)
Press the ENT Key to acknowledge the startup screen.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
6)
Appendix
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
Index
12) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
126
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
Flight
Instruments
13) Turn system power OFF.
14) Remove the SD card from the top card slot of the MFD.
15) Turn system power ON.
EIS
16) Press the ENT Key to acknowledge the startup screen.
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
Nav/Com/
XPDR/Audio
18) Turn the small FMS Knob to select the System Status Page.
AFCS
19) Press the Display Database Selection Softkey to show standby navigation
database information for each display (MFD1 DB, PFD1 DB, PFD2 DB).
Verify the correct standby navigation database cycle information is shown
for each display.
GPS Nav
To Manually Activate the Standby Navigation Database:
1) From the AUX-SYSTEM STATUS Page, select the STANDBY DB Softkey.
2) A prompt similar to the following figure below is displayed. Select ‘Yes’
to overwrite the Active Navigation Database with the Standby Navigation
Database. Select ‘No’ to cancel.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Standby Nav Database Activation Confirmation Window
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
127
Loading the Magnetic Field Variation Database update:
A copy of the current magnetic field variation database (MV DB) is included with
the navigation database. At startup, the system compares this version of the MV
DB with that presently being used by each AHRS (GRS1 and GRS2). If the system
determines the MV DB needs to be updated, a prompt is displayed on the Navigation
Map Page, as shown in the following figure.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
GRS1 Magnetic Field Variation Database Update Prompt
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
1)
Abnormal
Operation
Uploading Database to GRS1
When the upload is complete, the prompt for the next GRS upload is
displayed.
Index
Appendix
Annun/
Alerts
2)
GRS2 Magnetic Field Variation Database Update Prompt
128
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Appendix
With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed. When the upload is complete, the system is ready for use.
Flight
Instruments
3)
EIS
Nav/Com/
XPDR/Audio
AFCS
Uploading Database to GRS2
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
129
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
Blank Page
130
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Index
AFCS
DB Mismatch 121
DCLTR Softkey 66
Dead Reckoning 80
Declutter 80, 113, 121
Designated altitudes 23
Direct-to 19
DME 11
DR mode 80, 81, 82
GPS Nav
Flight
Planning
E
Procedures
Edit a flight plan 39
Electronic checklists 74, 75
Electronic Stability 77
Emergency checklist 75
Engine display 7
ESP 77
Hazard
Avoidance
Additional
Features
F
Gain 61
Ground mapping 61
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index
CDI 3, 11, 108
Channel Presets 70
Appendix
G
Annun/
Alerts
C
Abnormal
Operation
Barometric Altitude Minimums 5
Barometric pressure 117
Bearing line 60, 61, 62
190-00645-08 Rev. A
Nav/Com/
XPDR/Audio
D
FD 88
Flight Director 15
Flight ID 56
Flight path marker 65
FliteCharts® 66, 67
Frequency Transfer 11
Fuel remaining 119
B
EIS
Activate a flight plan 20
Active Channel 69
Active database 124
Active Navigation Database 123
ADF 11
Advisory alerts 85
AHRS 101, 102, 103, 105
Aircraft alerts 83
Air Data Computer 87
Airport Directory 68
Airport Signs 65, 66
Airways 120
ALT 55
Altimeter setting 1, 80
Altitude mode 55
Altitude volume 55
Antenna stabilization 62
Antenna tilt 60
AP 88
Attitude & Heading Reference System
87
Audio entertainment 69
Audio panel controls
NAV1, NAV2 11
Aural alerts 85
Automatic Flight Control System (AFCS)
Alerts 88
ChartView 66, 67
Checklists 74, 75
Clearance player 12
Clearance recorder 12
Code selection softkeys 11
COM 11, 12, 79
Flight
Instruments
A
Index-1
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
H
Horizon heading 65
Horizontal scan 61
I
Inhibit 59
Inhibit TAWS 59
Inset Map 113, 114
Intercom isolation 13
IOI 89
Navigation database 21, 23, 111
NEXRAD 51, 114, 120
O
OBS 3
Obstacles 95, 96, 98
Overspeed Protection 16
P
J
Pathways 65, 66
PIT 86, 87
Power-up page 74
Jeppesen 67
R
L
Reversionary mode 79
ROC 89
Lightning 50, 114
M
Maintenance 71, 72
Map panning 52
Message advisories 90, 92, 96, 101,
103, 105, 106
MET 88
METAR 51
Minimums 85
MISCOMP 86, 87
MKR/MUTE 12
Mode S 118
Mode selection softkeys 11
Multi Function Display (MFD)
Softkeys 119
N
NAV 11
NAV1 3, 11
NAV2 3, 11
Index-2
S
SafeTaxi® 66
SBAS 44, 59, 81, 98, 99
Scheduler 72
SD Card 121, 122, 124, 125, 126, 127
Sector scan 62
Secure Digital (SD) card 74
Sensor 87
SiriusXM Lightning 114, 120
SiriusXM Radio 69
SiriusXM Weather 52
STAB 62
Standby 60
Standby Navigation Database 125, 127
Store Flight Plan 39
Stormscope lightning data 49, 50, 114
Supplemental Data Card 122, 123
SVS 65, 109
Synchronization 122
Synthetic Vision System 65
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Index
Flight
Instruments
T
EIS
TA 85, 86
TAF 51
TAS 55, 56, 101
TAWS 58, 59, 89
TAWS-B 58
Terrain 58, 95, 114, 120
Tilt line 60
Timer 4
Topographical data 114, 120
Traffic 49, 54, 120
Traffic Advisory 54, 86
Traffic Advisory (TA) 85, 86
Traffic map page 54, 55, 56
Transponder 11, 117, 118
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
V
Procedures
Vertical speed guidance 23
Vertical track 85
Video display 76, 77
Video settings 76
VNAV 108
VNV 19, 80
Hazard
Avoidance
Additional
Features
W
Abnormal
Operation
WATCH® 62
Waypoint Selection Submenu 32, 33
Weather Attenuated Color Highlight 62
Weather data link page 52
Weather radar 59
Wind data 116
Annun/
Alerts
Appendix
Index
190-00645-08 Rev. A
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK® 100
190-00645-08 Rev. A
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR, U.K.
p: 44 (0) 23 8052 4000 f: 44 (0) 23 8052 4004
Aviation Support: 44 (0) 87 0850 1243
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2007-2010, 2012, 2014, 2015 Garmin Ltd. or its subsidiaries
190-00645-08 Rev. A
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