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Garmin G1000: Quest Kodiak 100, G1000 - Quest Kodiak 100 Reference guide

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Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
p:44 (0) 23 8052 4000
f:44 (0) 23 8052 4004
Aviation Support:44 (0) 87 0850 1243
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
www.garmin.com
Quest KODIAK
®
100
G1000
®
Integrated Avionics System
Pilot’s Guide
G1000
®
Pilot’s Guide
Quest KODIAK
®
100
190-00590-07
Revision A
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
190-00590-08 Rev. A
Copyright © 2006-2012, 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.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax: 503/364.2138
Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K
Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004 Aviation Support:44 (0) 87 0850 1243
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Website Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin
®
and G1000
®
are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts
®
, SafeTaxi
®
, and Garmin ESP
™
are trademarks
of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
Bendix/King
®
and Honeywell
®
are registered trademarks of Honeywell International, Inc.; NavData
®
is a registered trademark of Jeppesen,
Inc.; Stormscope
®
is a registered trademark of L-3 Communications; Avidyne
®
and TCAD
®
are registered trademarks of Avidyne Corporation;
and KODIAK
®
is a registered trademark of Quest Aircraft Compapny. SiriusXM Weather and SiriusXM Satellite Radio are provided by
SiriusXM Satellite Radio, Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
July 2015 Printed in the U.S.A
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
i
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance
feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74 Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering.
The traffic display does not provide collision avoidance resolution advisories and does not under any
circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.
WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic
within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information
from aircraft or ground stations, traffic may be present that is not represented on the display.
WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous
weather avoidance. Range limitations and interference may cause the system to display inaccurate or
incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be significantly older than the indicated weather product age.
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
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190-00590-08 Rev. Aii
WARNINGS, CAUTIONS, AND NOTES
WARNING:
For safety reasons, G1000 operational procedures must be learned on the ground.
WARNING:
The Garmin system, as installed in this aircraft, has a very high degree of functional integrity.
However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable
system failures is not practical.
WARNING:
The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING:
To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Airplane Flight Manual.
Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications
from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual
sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
WARNING: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are
only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information
Manual (AIM) recommend avoiding any thunderstorm identified as severe of giving intense radar echo by
at least 20 miles.
WARNING
:
Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING
:
Because of variation in the earth’s magnetic field, operating the system within the following
areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all
longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude
75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W.
(Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia);
South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New
Zealand)
WARNING
:
Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
WARNING
: Do not use a QFE altimeter setting with this system. System functions will not operate properly
with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the
standard pressure setting, as applicable.
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
iii
WARNINGS, CAUTIONS, AND NOTES
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
CAUTION:
The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby
thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of
two or more discharge points in the strike display mode do indicate thunderstorm activity if these points
reappear after the screen has been cleared.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and
displays, are subject to change and may not reflect the most current G1000 system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
NOTE
: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE
: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards
away from the source of the interference should alleviate the condition.
NOTE
: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE
: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
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190-00590-08 Rev. Aiv
WARNINGS, CAUTIONS, AND NOTES
NOTE
: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the
following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information
related to the use of databases in the National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases
obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue
of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database
and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with
established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures
that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.
NOTE
: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed
in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at
www.flygarmin.com by selecting ‘Database Exclusions List.’
NOTE
: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their
impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by
selecting ‘Aviation Database Alerts.’
NOTE
: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to
coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select ‘Report An Aviation Data Error Report.’
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
v
REVISION INFORMATION
Record of Revision
Part Number Revision Date Page Range Description
190-00590-00
190-00590-00
190-00590-00
A
B
C
3/21/07
4/3/07
6/22/07
All
All
All
Initial Release
Added Print Specification Reference to Cover Sheet
Revised AMPS Engine Gauge
190-00590-01 A 10/13/08 All Added GDU 8.20 parameters including gradient PFD
Added WAAS
Revised Flight Instruments/Annunciations
Added Weight Planning Page
Rewrote GPS Nav section to become Flight Management section
Added FliteCharts, ChartView, and SafeTaxi
Corrected various clerical errors
Changes for new book format
Added GDU 9.03 changes
Added SVS
190-00590-02 A 7/31/09 All Added GDU 9.1x changes
Added GDU 10.00 changes
Corrected various clerical errors
190-00590-03 A 5/7/10 All Added TKS Ice Protection Indications
Updated wind options
Enabled groundspeed and current track line on PFD
190-00590-04 A 11/5/10 All Updated Ice Protection display on the Engne System Page
Updated CAS messages
190-00590-05 A 1/6/12 All Added GWX 68
Added GTS 800
Updated CAS messages
- Remove Bleed Air On and Aux Bus On advisory annunciations
- Add AIR COND INH annunciation
Added Dynamic reference approach speed (green circle)
190-00590-06 A 3/12/14 All Added GDU 12.10, 13.0, & 14.01 changes
Added Garmin AFCS
Added Garmin ESP
Added Maintenance Log feature
Added AC-U-KWIK Airport Directory
Added User Defined Holding Patterns
Added Temperature Compensated Altitudes
Added Weather Radar Overlay
Added Profile View
Updated system messages
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
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190-00590-08 Rev. Avi
REVISION INFORMATION
190-00590-06 B 5/1/14 All Changed KODIAK
™
to KODIAK
®
Incorporated Quest comments on the Garmin AFCS
-
Removed automatic activation of Low Bank Mode
-
GA switch does not uncouple autopilot
-
Roll Trim does not uncouple autopilot
Corrections to USP and ESP
Added Database notes
Updated System Software Number for GDU 14.02
190-00590-07 A 8/29/14 All
Corrected Underspeed Protection CAS Warning
Added AFCS Config CAS Warning
Added AFCS Config alerts window message
Corrected CRG part number on Aux System Status Page
Updated System Software Number
190-00590-08 A 7/21/15 All
Updated to GDU 14.04
Updated to GDL 69A SXM
Updated Fuel Indications
Updated CAS Messages
Updated System Software Number
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
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vii
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ................................................. 1
1.2 Line Replaceable Units ........................................... 2
1.3 G1000 Controls ........................................................ 6
PFD/MFD Controls ........................................................ 6
Controls Associated With the MFD ................................. 8
Audio Panel Controls .................................................... 9
1.4 Secure Digital (SD) Cards .....................................11
1.5 System Power-Up .................................................. 12
1.6 System Operation .................................................. 13
Normal Display Operation ........................................... 13
Reversionary Mode ..................................................... 13
AHRS Operation ......................................................... 14
G1000 System Annunciations ...................................... 16
Softkey Function ......................................................... 17
GPS Receiver Operation .............................................. 23
1.7 Accessing G1000 Functionality............................ 28
Menus ....................................................................... 28
Data Entry.................................................................. 28
MFD Page Groups ....................................................... 29
System Setup and Status ............................................. 32
1.8 Display Backlighting ............................................. 49
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................. 54
Airspeed Indicator ...................................................... 54
Attitude Indicator ....................................................... 56
Altimeter ................................................................... 57
Vertical Speed Indicator (VSI) ....................................... 61
Vertical Deviation ....................................................... 61
Horizontal Situation Indicator (HSI) .............................. 62
Course Deviation Indicator (CDI) .................................. 67
2.2 Supplemental Flight Data .................................... 75
Temperature Displays .................................................. 75
Wind Data ................................................................. 76
Vertical Navigation (VNV) Indications ........................... 77
2.3 PFD Annunciations and Alerting Functions ........ 78
System Alerting .......................................................... 78
Marker Beacon Annunciations...................................... 79
Traffic Annunciation .................................................... 80
TAWS Annunciations ................................................... 81
Altitude Alerting ......................................................... 81
Low Altitude Annunciation .......................................... 82
Minimum Descent Altitude/Decision Height Alerting ...... 82
2.4 Abnormal Operations ........................................... 84
Abnormal GPS Conditions ........................................... 84
Heading Failure Modes................................................ 85
Unusual Attitudes ....................................................... 85
SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1 Engine Display ....................................................... 90
3.2 System Display ...................................................... 92
3.3 Fuel Display ............................................................ 94
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ................................................................ 97
MFD/PFD Controls and Frequency Display ..................... 98
Audio Panel Controls ................................................ 100
4.2 COM Operation .................................................... 102
COM Transceiver Selection and Activation ................... 102
COM Transceiver Manual Tuning ................................ 103
Quick-tuning and Activating 121.500 MHz .................. 104
Auto-tuning the COM Frequency ................................ 105
Frequency Spacing .................................................... 109
Automatic Squelch .................................................... 110
Volume .................................................................... 110
4.3 NAV Operation ..................................................... 111
NAV Radio Selection and Activation ........................... 111
NAV Receiver Manual Tuning ..................................... 112
Auto-tuning a NAV Frequency from the MFD ............... 114
Auto-tuning NAV Frequencies on Approach Activation . 118
Marker Beacon Receiver ............................................ 119
4.4 GTX 33 Mode S Transponder .............................. 120
Transponder Controls ................................................ 120
Transponder Mode Selection ...................................... 121
Entering a Transponder Code ..................................... 124
IDENT Function ........................................................ 125
4.5 Additional Audio Panel Functions ..................... 126
Power-up ................................................................. 126
Mono/Stereo Headsets .............................................. 126
Speaker ................................................................... 126
Intercom .................................................................. 127
Passenger Address (PA) System .................................. 129
Garmin G1000 Pilot’s Guide for the Quest KODIAK
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190-00590-08 Rev. Aviii
TABLE OF CONTENTS
Simultaneous COM Operation .................................... 129
Clearance Recorder and Player ................................... 130
Entertainment Inputs ................................................ 131
4.6 Audio Panels Preflight Procedure ...................... 132
4.7 Abnormal Operation ........................................... 134
Stuck Microphone ..................................................... 134
COM Tuning Failure ................................................... 134
PFD Failure, Dual System ........................................... 135
Audio Panel Fail-safe Operation ................................. 136
Reversionary Mode ................................................... 136
SECTION 5 FLIGHT MANAGEMENT
5.1 Introduction ......................................................... 137
Navigation Status Box ............................................... 138
5.2 Using Map Displays ............................................. 140
Map Orientation ....................................................... 140
Map Range .............................................................. 142
Map Panning ............................................................ 144
Measuring Bearing and Distance ................................ 148
Topography .............................................................. 149
Map Symbols ........................................................... 152
Airways ................................................................... 158
Track Vector ............................................................. 160
Wind Vector ............................................................. 161
Nav Range Ring........................................................ 162
Fuel Range Ring ....................................................... 163
Field of View (SVT) .................................................... 164
Selected Altitude Intercept Arc ................................... 165
5.3 Waypoints ............................................................. 166
Airports ................................................................... 167
Intersections ............................................................ 174
NDBs ....................................................................... 176
VORs ....................................................................... 178
User Waypoints ........................................................ 180
5.4 Airspaces .............................................................. 186
5.5 Direct-to-Navigation .......................................... 190
5.6 Flight Planning ..................................................... 195
Flight Plan Creation .................................................. 196
Adding Waypoints to an Existing Flight Plan ................ 201
Adding Airways to a Flight Plan ................................. 203
Adding Procedures to a Stored Flight Plan .................. 205
Flight Plan Storage ................................................... 212
Flight Plan Editing .................................................... 214
Along Track Offsets ................................................... 217
Parallel Track ............................................................ 219
Activating a Flight Plan Leg ....................................... 222
Inverting a Flight Plan ............................................... 223
Flight Plan Views ...................................................... 224
Closest Point of FPL .................................................. 226
User-Defined Holding Patterns ................................... 226
5.7 Vertical Navigation ............................................. 231
Altitude Constraints .................................................. 233
5.8 Procedures ...........................................................237
Departures ............................................................... 238
Arrivals ................................................................... 241
Approaches ............................................................. 244
5.9 Trip Planning ........................................................ 252
Trip Planning ............................................................ 252
Weight Planning ....................................................... 256
Weight Caution And Warning Conditions .................... 258
5.10 RAIM Prediction................................................... 259
5.11 Navigating a Flight Plan ..................................... 262
5.12 Abnormal Operation ........................................... 290
SECTION 6 HAZARD AVOIDANCE
6.1 SiriusXM Weather ................................................ 294
Using SiriusXM Weather Products .............................. 296
6.2 Airborne Color Weather Radar .......................... 328
System Description ................................................... 328
Principles of Pulsed Airborne Weather Radar ............... 328
Safe Operating Distance ............................................ 332
Basic Antenna Tilt Setup ............................................ 333
Weather Mapping and Interpretation ......................... 334
Ground Mapping and Interpretation ........................... 346
Weather Radar Overlay on the Navigation Map Page ... 347
System Status ........................................................... 349
6.3 WX-500 Stormscope ........................................... 350
Setting Up Stormscope on the Navigation Map ........... 350
Selecting the Stormscope Page .................................. 354
6.4 TAWS-B ................................................................. 355
TAWS-B Page ........................................................... 359
TAWS-B Alerts .......................................................... 360
System Status ........................................................... 367
6.5 Profile View Terrain ............................................. 369
Profile View Display .................................................. 370
190-00590-08 Rev. A
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ix
TABLE OF CONTENTS
6.6 Traffic Information Service (TIS) ........................ 372
Displaying Traffic Data .............................................. 373
Traffic Map Page ....................................................... 375
TIS Alerts ................................................................. 376
System Status ........................................................... 377
6.7 Garmin GTS 800 Traffic ....................................... 380
Theory of Operation .................................................. 380
TAS Alerts ................................................................ 382
System Test .............................................................. 383
Operation ................................................................ 384
System Status ........................................................... 390
6.8 SKY497 Traffic ...................................................... 392
TAS Symbology ......................................................... 392
Operation ................................................................ 393
Altitude Display ........................................................ 396
Traffic Map Page Display Range ................................. 396
TAS Alerts ................................................................ 398
System Status ........................................................... 398
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 Garmin AFCS ........................................................ 401
Basic Autopilot Operation .......................................... 402
Garmin AFCS Controls ............................................... 403
Flight Director Operation ........................................... 405
Vertical Modes ......................................................... 408
Lateral Modes .......................................................... 422
Autopilot and Yaw Damper Operation ........................ 428
Level Mode .............................................................. 430
Underspeed Protection .............................................. 431
Flap Configuration Trim (FCT) ..................................... 433
Example Flight Plan .................................................. 433
AFCS Annunciations and Alerts .................................. 445
Abnormal Operation ................................................. 447
7.2 S-TEC Fifty Five X Autopilot (Optional) ............ 448
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision Technology (SVT
™
) .................. 450
SVT Operation .......................................................... 451
SVT Features ............................................................ 453
Field of View ............................................................ 462
8.2 SafeTaxi ................................................................ 464
SafeTaxi Cycle Number and Revision .......................... 467
8.3 ChartView ............................................................. 470
ChartView Softkeys ................................................... 471
Terminal Procedures Charts ....................................... 472
Chart Options ........................................................... 480
Day/Night View ........................................................ 486
ChartView Cycle Number and Expiration Date ............. 488
8.4 FliteCharts ............................................................ 491
FliteCharts Softkeys .................................................. 492
Terminal Procedures Charts ....................................... 493
Chart Options ........................................................... 500
Day/Night View ........................................................ 504
FliteCharts Cycle Number and Expiration Date ............. 506
8.5 Airport Directory ................................................. 509
Airport Directory Database Cycle Number and Revision 510
8.6 SiriusXM Satellite Radio (Optional) .................. 512
Activating SiriusXM Satellite Radio Services ................ 512
Using SiriusXM Satellite Radio ................................... 514
8.7 Maintenance Logs ............................................... 517
8.8 Scheduler .............................................................. 522
8.9 Electronic Checklists ........................................... 524
8.10 Flight Data Logging ............................................ 527
8.11 Auxiliary Video ..................................................... 529
Video Setup .............................................................530
Display Selection ...................................................... 530
Input Selection ......................................................... 531
Zoom/Range ............................................................ 532
8.12 Electronic Stability & Protection (ESP
™
) ........... 533
Roll Engagement ...................................................... 534
Pitch Engagement..................................................... 536
High Airspeed Protection ........................................... 536
8.13 Abnormal Operation ........................................... 537
SVT Troubleshooting ................................................. 537
Reversionary Mode ................................................... 537
Unusual Attitudes ..................................................... 538
APPENDICES
Annunciations and Alerts ............................................. 541
Alert Level Definitions ............................................... 542
Aircraft Alerts ........................................................... 543
Comparator Annunciations ........................................ 546
G1000 System Annunciations .................................... 548
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
190-00590-08 Rev. Ax
TABLE OF CONTENTS
G1000 System Message Advisories ............................. 550
AFCS Alerts .............................................................. 564
TAWS-B ALERTS ........................................................ 565
TAWS-B System Status Annunciations ......................... 565
Flight Plan Import/Export Messages ........................... 566
Pilot Profile Import/Export Messages .......................... 567
Database Management ................................................ 569
Jeppesen Databases .................................................. 570
Garmin Databases .................................................... 573
Garmin Aviation Glossary ............................................ 581
Frequently Asked Questions ........................................ 589
General TIS Information ............................................... 593
Introduction ............................................................. 593
TIS vs. TAS/TCAS ....................................................... 593
TIS Limitations.......................................................... 593
Map Symbols ................................................................. 595
INDEX
Index ................................................................................ I-1
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
1
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& cNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section is designed to provide an overview of the G1000 Integrated Flight Deck installed in the Quest
KODIAK
®
100. The G1000 is an integrated flight deck system that presents flight instrumentation, position,
navigation, communication, and identification information to the pilot using flat-panel color displays. The
system is distributed across the following Line Replaceable Units (LRUs):
•
GDU 1040
Primary Flight Display (PFD)/Multi
Function Display (MFD)
•
GMA 1347
Audio Panel with Integrated Marker
Beacon Receiver
•
GIA 63W
Integrated Avionics Units (IAU)
•
GDC 74A
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GTX 33
Mode S Transponder
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GDL 69A/69A SXM
Data Link Receiver (Optional)
•
GWX 68
Weather Radar (Optional)
•
GTS 800
Traffic Avoidance System (Optional)
•
GMC 710
AFCS Control Unit (Optional)
•
GSA 80/81
AFCS Servos (Optional)
•
GSM 86
Servo Gearboxes (Optional)
A top-level G1000 system block digram is shown in Figure 1-1 (it does not include the GSM 86).
NOTE: Refer to the AFCS section for details on the Garmin AFCS.
The Garmin Automated Flight Control System (AFCS) provides the flight director (FD) and autopilot (AP)
functions of the G1000 system.
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
190-00590-08 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
2
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.2 LINE REPLACEABLE UNITS
• GDU 1040 (3) – The GDU 1040 is configured as two Primary Flight Displays (PFD) and one Multi Function
Display (MFD). The displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet
connection. Each display is also paired with an Ethernet connection to an IAU.
•
GMA 1347
(2) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,
intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual
control of display reversionary mode (red
DISPLAY BACKUP
Button; see Section 1.5, System Operation) and
communicates with both IAUs using an RS-232 digital interface.
•
GIA 63W
(2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all
LRUs with the PFD. Each IAU contains VHF COM/NAV/GS receivers and system integration microprocessors
and is paired with the on-side display via an HSDB connection. The IAUs are not paired together and do not
communicate with each other directly.
•
GDC 74A
(2) – The Air Data Computer (ADC) processes data from the pitot/static system and outside air
temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information
to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429
digital interface.
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
3
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& cNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
•
GEA 71
(1) – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors.
This unit communicates with both IAUs using an RS-485 digital interface.
•
GTX 33
(1) – The solid-state Transponder provides Modes A, C, and S capability and communicates with both
IAUs through an RS-232 digital interface.
•
GRS 77
(2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors
(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation
is discussed in Section 1.5, System Operation.
•
GMU 44
(2) – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.
•
GDL 69A/69A SXM
(1) – The Data Link Satellite Radio Receiver provides real-time weather information to the
G1000 MFD and PFD Inset Map, as well as digital audio entertainment. The Data Link Receiver communicates
with the MFD via an HSDB connection. A subscription to XM Satellite Radio Service is required to enable the
GDL 69A capability.
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
190-00590-08 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
4
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
•
GWX 68
(1)(optional) – Provides airborne weather and ground mapped radar data to the MFD via HSDB
connection.
•
GTS 800
(optional) – The GTS 800 Traffic Advisory System (TAS) uses active interrogations of Mode S and
Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system.
•
GSA 80
(2),
GSA 81
(2), and
GSM 86
(4) (optional) – The GSA 80 servos are used for the automatic control
of pitch and yaw. The GSA 81 servos are used for the automatic control of roll and pitch trim. These units
interface with each GIA 63W.
The GSM 86 servo gearboxes are responsible for transferring the output torque of the GSA 80/81 servo actuators
to the mechanical flight-control surface linkage.
•
GMC 710
(1) (optional) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface
allowing communication with both PFDs.
190-00590-08 Rev. A
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
5
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& cNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
GMA 1347
Audio Panel #2
GTX 33
Transponder
GEA 71
Engine/
Airframe Unit
GDC 74A #1
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GMU 44 #1
Magnetometer
Heading
GMA 1347
Audio Panel #1
GDU 1040
PFD #1
GDU 1040
MFD
GMC 710
AFCS Control Unit (optional)
GDU 1040
PFD #2
GRS 77 #1
AHRS
Attitude
Rate of Tu rn
Slip/Skid
GDC 74A #2
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
GMU 44 #2
Magnetometer
Heading
#
2
e
d
GRS 77 #2
AHRS
Attitude
Rate of Tu rn
Slip/Skid
GIA 63W #2
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
GPS Output
L-3 Skywatch
SKY497
Traffic
Advisory System
(optional)
L-3 WX-500
Stormscope
Lightning Sensor
(optional)
GDL 69A/
69A SXM
Data Link
Real-time Weather
and Digital Audio
Entertainment
(optional)
GWX 68
Weather Radar
Airborne Weather
and Ground Mapped
Radar Data
(optional)
GIA 63W #1
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
GPS Output
GD
V
G
M
G
R
We
a
nd
GTS 800
Traffic Advisory
System
(optional)
GSA 80 (2)
GSA 81 (2)
Servos
(optional)
Figure 1-1 Basic G1000 System Block Diagram
Garmin G1000 Pilot’s Guide for the Quest KODIAK
®
100
190-00590-08 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
6
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section.
The G1000 system controls are located on the PFD and MFD bezels and the audio panel. The controls for the
PFD and MFD are discussed within the following pages of this section.
PFD/MFD CONTROLS
Figure 1-2 PFD/MFD Controls
1718
5
6
8
7
2
4
31 9
15
14
13
12
16
11
10
The NAV, CRS/BARO, COM, FMS, and ALT Knobs are concentric dual knobs, each having small (inner)
and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used.
Large (Outer)
Knob
Small (Inner)
Knob
Figure 1-3 Dual Concentric Knob
/