Garmin G500H PILOT'S GUIDE
G500H
Pilot's Guide
© 2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 4.00, or later. Some differences in operation
may be observed when comparing the information in this manual to later software versions.
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Tel: 913/397.8200 Fax: 913/397.8282
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April 2010 Printed in the U.S.A.
AVIATION LIMITED WARRANTY
All Garmin avionics products are warranted to be free from defects in materials or workmanship for:
two years from the date of purchase for new Remote-Mount and Panel-Mount products; one year
from the date of purchase for new portable products and any purchased newly-overhauled products;
six months for newly-overhauled products exchanged through a Garmin Authorized Service Center;
and 90 days for factory repaired or newly-overhauled products exchanged at Garmin in lieu of repair.
Within the applicable period, Garmin will, at its sole option, repair or replace any components that
fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts
or labor, provided that the customer shall be responsible for any transportation cost. This warranty
does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts,
such as batteries, unless product damage has occurred due to a defect in materials or workmanship;
(iii) damage caused by accident, abuse, misuse, water, flood, fire, or other acts of nature or external
causes; (iv) damage caused by service performed by anyone who is not an authorized service
provider of Garmin; or (v) damage to a product that has been modified or altered without the written
permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against
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THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER
WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING
UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE,
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DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR
FROM DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR
CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement
product) the product or software or offer a full refund of the purchase price at its sole discretion.
SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
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will not replace missing components from any package purchased through an online auction.
International Purchases: A separate warranty may be provided by international distributors for
devices purchased outside the United States depending on the country. If applicable, this warranty is
provided by the local in-country distributor and this distributor provides local service for your device.
Distributor warranties are only valid in the area of intended distribution. Devices purchased in the
United States or Canada must be returned to the Garmin service center in the United Kingdom, the
United States, Canada, or Taiwan for service.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in
locating a Service Center near you, visit the Garmin web site at http://www.garmin.com or contact
Garmin Customer Service at 800-800-1020.
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
Garmin G500H Pilot’s Guide
i190-01150-02 Rev. B
Foreword
Sec 1
System
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
WARNING: Navigation and terrain separation must NOT be predicated
upon the use of the terrain function. The G500H Terrain Proximity feature
is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of
surroundings during flight. The Terrain Proximity feature is only to be used
as an aid for terrain avoidance and is not certified for use in applications
requiring a certified terrain awareness system. Terrain data is obtained
from third party sources. Garmin is not able to independently verify the
accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: The Garmin G500H 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 G500H. 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.
Sec 6
Annun.
Sec 7
Sec 8
Appendix B
& Alerts
Symbols
GlossaryAppendix A
Index
ii
WARNING: The altitude calculated by GPS receivers is geometric height
above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the output from the GDC 74H Air
Data Computer, or other altimeters in aircraft. GPS altitude should never
be used for vertical navigation. Always use pressure altitude displayed by
the G500H PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used
in the G500H system must be updated regularly in order to ensure that
the information remains current. Pilots using an 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.
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
WARNING: Traffic information shown on the G500H Multi Function Display
is provided as an aid in visually acquiring traffic. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition
of conflicting traffic.
WARNING: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69/69A is approved
only for weather avoidance, not penetration.
WARNING: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: For safety reasons, G500H operational procedures must be
learned on the ground.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G500H Pilot’s Guide. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully
compare indications from the G500H 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.
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
WARNING: Never use the G500H to attempt to penetrate a thunderstorm.
Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s
Information Manual (AIM) recommend avoiding “by at least 20 miles any
thunderstorm identified as severe or giving an intense radar echo.”
WARNING: Exceeding 200 deg/second in pitch or roll may invalidate
AHRS attitude provided to the G500H.
Garmin G500H Pilot’s Guide
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
iii190-01150-02 Rev. B
Foreword
Sec 1
System
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
Sec 6
Annun.
& Alerts
WARNING: Because of anomalies in the earth’s magnetic field, operating
the G500H within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude and between longitude 75°
West and 120° West. An area north of 70° North latitude and between
longitude 70° West and 128° West. An area north of 70° North latitude and
between longitude 85° East and 114° West. An area south of 55° South
latitude between longitude 120° East and 165° East.
WARNING: Do not use Terrain-HSVT information for primary terrain
avoidance. Terrain-HSVT is intended only to enhance situational
awareness.
CAUTION: 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 G500H utilize
GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as
with all NAVAIDs, information presented by the G500H can be misused or
misinterpreted and, therefore, become unsafe.
CAUTION: The Garmin G500H 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.
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Index
Appendix B
iv
CAUTION: The G500H 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.
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 feet away
from the source of the interference should alleviate the condition.
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
NOTE: All visual depictions contained within this document, including
screen images of the G500H bezel and displays, are subject to change and
may not reflect the most current GDU 620 system. Depictions of equipment
may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause
harmful interference, and (2) this device must accept any interference
received, including interference that may cause undesired operation.
NOTE: Terrain data is not displayed when the aircraft latitude is greater
than 75° North or 60° South.
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.
NOTE: Terrain-HSVT is standard when the Garmin Synthetic Vision
Technology™ (SVT) option is installed.
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Garmin G500H Pilot’s Guide
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
v190-01150-02 Rev. B
Foreword
Sec 1
System
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
Record of Revisions
Part Number Revision Date Description
190-01150-02 A 1/27/10 Production release
B 4/1/10 Update Airspeed Tape markings.
Sec 6
Annun.
Sec 7
Sec 8
Appendix B
& Alerts
Symbols
GlossaryAppendix A
Index
vi
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
Contents
1 System Overview .................................................................................1-1
1.1 System Description ................................................................................ 1-1
1.1.1 Line Replaceable Units (LRU) .................................................1-2
1.1.2 GDU 620 .............................................................................. 1-3
1.1.3 GDC 74H ..............................................................................1-3
1.1.4 GRS 77H ............................................................................... 1-4
1.1.5 GMU 44 ................................................................................ 1-4
1.1.6 GTX 330/330D (Optional) ......................................................1-5
1.1.7 GTP 59 ................................................................................. 1-5
1.1.8 GSR 56 .................................................................................1-5
1.1.9 GDL 69/69A (Optional) ..........................................................1-6
1.1.10 Garmin Navigator Interface .................................................... 1-6
1.1.11 Attitude Heading Reference System (AHRS) ............................ 1-7
1.1.12 Secure Data Cards ................................................................. 1-8
1.1.13 Pilot Controls ........................................................................1-9
1.1.13.1 PFD Knob ..............................................................................1-9
1.1.13.2 PFD Bezel Keys ....................................................................1-10
1.1.13.3 PFD Soft Keys ......................................................................1-11
1.1.13.4 MFD Knobs .........................................................................1-13
1.1.13.5 MFD Bezel Keys ................................................................... 1-13
1.1.13.6 MFD Soft Keys ..................................................................... 1-14
1.2 System Power Up ................................................................................ 1-15
1.2.1 International Geomagnetic Reference Field ..........................1-16
1.3 System Operation ................................................................................1-17
1.3.1 Using the Page Menus ......................................................... 1-17
1.3.1.1 Navigating within a Menu ................................................... 1-17
1.3.2 Using the Soft Key Controls .................................................1-18
1.3.3 System Settings ................................................................... 1-18
1.3.4 Display Backlighting ............................................................1-21
2 Primary Flight Display (PFD) ................................................................2-1
2.1 PFD Soft Key Map ................................................................................. 2-2
2.2 Airspeed Indicator ................................................................................. 2-2
2.2.1 Markings ............................................................................... 2-3
2.2.2 Reference Speeds ..................................................................2-4
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
Garmin G500H Pilot’s Guide
vii190-01150-02 Rev. B
2.3 Attitude Indicator .................................................................................. 2-4
2.3.1 Extreme Attitude ...................................................................2-6
2.4 Altimeter ..............................................................................................2-8
Foreword
2.4.1 Setting the Altitude Bug and Alerter ....................................... 2-8
2.4.2 Altitude Alerting ....................................................................2-9
2.4.3 Changing Barometric Setting .................................................2-9
Sec 1
System
2.4.4 Minimum Descent Altitude/Decision Height Alerting .............2-10
2.5 Vertical Speed (V/S) Indicator ..............................................................2-12
2.6 Horizontal Situation Indicator .............................................................. 2-13
PFD
Sec 2
2.6.1 Setting the Heading Bug ...................................................... 2-14
2.6.2 Turn Rate Indicator ..............................................................2-15
2.7 Course Deviation Indicator .................................................................. 2-15
2.7.1 Changing CDI Sources ......................................................... 2-16
MFD
Sec 3
2.7.2 Changing CDI Course ..........................................................2-17
2.7.3 Vertical Deviation Indicator (VDI) .........................................2-18
Sec 4
Hazard
2.7.4 Auto-Slewing ......................................................................2-19
Avoidance
2.8 Supplemental Flight Data .................................................................... 2-21
2.8.1 Bearing Pointers .................................................................. 2-21
2.8.2 Temperature Display ............................................................ 2-23
Sec 5
Features
2.9 Wind Vectors ...................................................................................... 2-23
Additional
2.10 Attitude (ATT) Sync ............................................................................. 2-24
3 Multi-Function Display (MFD) ..............................................................3-1
Sec 6
Annun.
3.1 Functional Display Map .........................................................................3-2
& Alerts
3.2 MFD Soft Key Map ................................................................................3-3
3.3 Navigation Map Pages ..........................................................................3-4
Sec 7
Sec 8
Appendix B
3.3.1 Default Navigation Map Page ................................................ 3-5
Symbols
3.3.2 Editing Information ................................................................ 3-5
3.3.3 Selecting Page Options ..........................................................3-5
3.3.4 Changing the Navigation Map Range ....................................3-5
GlossaryAppendix A
3.3.5 Decluttering Map Pages .........................................................3-6
3.3.7 Selecting Items on the Map ...................................................3-9
3.3.8 Measuring Distances ...........................................................3-10
3.3.9 Customizing Navigation Map Pages ..................................... 3-11
3.3.10 Map Setup ..........................................................................3-11
3.3.10.1 Map Feature Options ........................................................... 3-13
Index
3.3.10.2 Weather Feature Options (Optional) .....................................3-28
3.3.10.3 Traffic Feature Options (Optional) ......................................... 3-31
viii
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
3.3.10.4 Aviation Feature Options ..................................................... 3-32
3.3.11 Split Screen (Optional) ......................................................... 3-43
3.4 Aux Mode Pages ................................................................................. 3-44
3.4.1 System Settings ................................................................... 3-44
3.4.1.1 Display Brightness ............................................................... 3-45
3.4.1.2 Airspeed Reference Marks ................................................... 3-46
3.4.1.3 PFD Options - Wind Vector ...................................................3-47
3.4.1.4 Date and Time ..................................................................... 3-48
3.4.1.5 MFD Display Units ............................................................... 3-49
3.4.1.6 System Display Units ...........................................................3-50
3.4.2 XM Information (Optional) ................................................... 3-51
3.4.3 XM Entertainment Radio (Optional) .....................................3-52
3.4.4 System Status ......................................................................3-53
3.4.5 External Video (optional) ......................................................3-54
3.4.5.1 Select Video Source .............................................................3-54
3.4.5.2 Zoom ..................................................................................3-55
3.4.5.3 Panning ..............................................................................3-55
3.4.5.4 Setup ..................................................................................3-55
3.4.5.5 Restore Defaults .................................................................. 3-57
3.4.6 Position Reporting (optional) ...............................................3-58
3.4.6.1 Status ................................................................................. 3-58
3.4.6.2 Report Type ......................................................................... 3-58
3.5 Flight Plan Pages ................................................................................ 3-61
3.5.1 Active Flight Plan Page ........................................................ 3-61
3.5.1.1 Active Flight Plan Detail .......................................................3-62
3.5.1.2 Active Flight Plan Options ....................................................3-62
3.5.1.3 Setting the Altitude Minimums Alerter .................................. 3-63
3.5.2 Waypoint Information Page .................................................3-64
3.5.2.1 Selecting a Waypoint ...........................................................3-65
3.5.2.2 Waypoint Information Detail ................................................3-67
3.5.2.3 Waypoint Weather Information (Optional) ............................ 3-70
3.5.3 Charts Page (Optional) ........................................................3-71
3.5.3.1 Viewing Charts ....................................................................3-72
3.5.3.2 Selecting a New Chart by Airport .........................................3-73
3.5.3.3 Selecting a New Chart by FPL, NRST, or RECENT ...................3-74
3.5.3.4 Change Day/Night View .......................................................3-74
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
Garmin G500H Pilot’s Guide
ix190-01150-02 Rev. B
4 Hazard Avoidance ................................................................................4-1
4.1 Terrain Configurations ........................................................................... 4-1
4.2 Terrain Proximity ................................................................................... 4-3
Foreword
4.2.1 Displaying Terrain Proximity ...................................................4-4
4.2.1.1 Terrain Proximity Page 120° Arc or 360° Rings ....................... 4-6
Sec 1
Sec 2
Sec 3
Sec 4
Hazard
Sec 5
Additional
Sec 6
Annun.
Sec 7
Sec 8
Appendix B
4.2.1.2 Terrain Proximity Page Aviation Data ...................................... 4-7
System
4.2.2 Terrain Proximity Limitations ..................................................4-9
4.2.3 System Status ........................................................................4-9
4.3 External H-TAWS ................................................................................. 4-10
PFD
4.4 Garmin Terrain-HSVT™ (Optional) ....................................................... 4-11
4.4.1.1 Garmin Terrain-HSVT™ Page 120° Arc or 360° Rings ..........4-12
4.4.1.2 Garmin Terrain-HSVT™ Page Aviation Data .........................4-13
MFD
4.4.1.3 Inhibiting/Enabling Garmin Terrain-HSVT™ Alerting .............4-14
4.4.1.4 Garmin Terrain-HSVT™ Reduce Protection (RP) Mode .......... 4-15
4.4.1.5 Synthetic Vision Alerts and Annunciations .............................4-17
4.4.1.6 Mute Caution Alerts ............................................................4-19
Avoidance
4.4.1.7 SVT Alerts When Terrain Inhibited ......................................... 4-20
4.5 TAS Traffic (Optional) ...........................................................................4-21
4.5.1 Displaying and Operating Traffic (TAS Systems) ..................... 4-21
Features
4.5.1.1 Switching from Standby Mode to Operating Mode ............... 4-21
4.5.1.2 Range Ring ......................................................................... 4-22
4.5.2 Altitude Display ................................................................... 4-23
4.5.3 TAS Symbology .................................................................... 4-24
& Alerts
4.5.4 Traffic System Status ............................................................ 4-25
4.5.5 Traffic Pop-Up......................................................................4-27
4.6 TIS Traffic (Optional) ............................................................................4-28
Symbols
4.6.1 Traffic Map Page..................................................................4-28
4.6.2 TIS Symbology ..................................................................... 4-30
4.6.3 TIS Limitations ..................................................................... 4-31
GlossaryAppendix A
4.6.4 TIS Alerts .............................................................................4-33
4.6.5 Traffic Pop-Up......................................................................4-34
4.6.6 TIS System Status ................................................................4-35
4.7 XM Weather (Optional) .......................................................................4-37
4.7.1 Using XM Satellite Weather Products ................................... 4-37
4.7.2 Customizing the XM Weather Map ......................................4-38
Index
4.7.3 XM Weather Symbols and Product Age ................................ 4-41
4.7.4 Weather Legends ................................................................4-43
x
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
4.7.5 NEXRAD ............................................................................. 4-44
4.7.5.1 Reflectivity ..........................................................................4-45
4.7.5.2 NEXRAD Limitations ............................................................ 4-46
4.7.6 Weather Page Map Orientation ............................................4-47
4.7.7 NEXRAD Data Viewing Range .............................................. 4-47
4.7.8 NEXRAD Legend.................................................................. 4-48
4.7.9 Echo Tops ............................................................................ 4-49
4.7.10 Cloud Tops .......................................................................... 4-51
4.7.11 XM Lightning ......................................................................4-53
4.7.12 Cell Movement ....................................................................4-54
4.7.13 SIGMETs and AIRMETs ........................................................4-56
4.7.14 METARs .............................................................................. 4-58
4.7.15 Surface Analysis and City Forecast ........................................ 4-60
4.7.16 Freezing Level......................................................................4-63
4.7.17 Winds Aloft ......................................................................... 4-65
4.7.18 County Warnings ................................................................. 4-68
5 Additional Features (Optional) ............................................................5-1
5.1 Viewing Charts .....................................................................................5-2
5.1.1 Chart Panning ....................................................................... 5-3
5.1.2 Choosing a Chart for the Current Airport ................................5-4
5.1.3 Selecting a Chart by Identifier ................................................ 5-5
5.1.4 Selecting a New Chart by FPL, NRST, or RECENT .....................5-6
5.1.5 Viewing Chart NOTAMs .........................................................5-7
5.1.6 Day/Night View ..................................................................... 5-7
5.2 ChartView ............................................................................................5-8
5.2.1 Cycle Number and Revision ...................................................5-8
®
5.3 FliteCharts
5.3.1 Cycle Number and Revision .................................................5-11
5.4 SafeTaxi
5.4.1 Using SafeTaxi
5.4.1.1 Decluttering ........................................................................ 5-14
5.4.1.2 Hot Spot Information ........................................................... 5-14
5.4.2 SafeTaxi
5.5 XM
®
5.5.1 Activating XM
5.5.2 XM
5.5.3 XM
....................................................................................... 5-11
®
..........................................................................................5-13
®
.................................................................5-14
®
Cycle Number and Revision .................................. 5-15
Radio Entertainment ..................................................................5-17
®
Satellite Radio Services ................................ 5-17
®
Information .................................................................5-19
®
Entertainment Radio ...................................................5-20
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
Garmin G500H Pilot’s Guide
xi190-01150-02 Rev. B
5.5.3.1 Channel Categories .............................................................5-21
®
5.5.3.2 Selecting an XM
5.5.3.3 XM
Foreword
5.5.3.4 XM
®
Radio Volume ..............................................................5-23
®
Radio Channel Presets ................................................. 5-24
Radio Channel ......................................... 5-22
5.5.4 GDL 69/69A Data Link Receiver Troubleshooting .................. 5-25
5.6 Garmin Synthetic Vision Technology (SVT™) (Optional) ........................5-26
Sec 1
System
5.6.1 Garmin SVT™ Operation ..................................................... 5-28
5.6.2 Activating and Deactivating Garmin SVT™ .......................... 5-29
5.6.3 Garmin SVT™ Features ....................................................... 5-30
PFD
Sec 2
5.6.3.1 Flight Path Marker (FPM) .....................................................5-30
5.6.3.2 Zero-Pitch Line .................................................................... 5-30
5.6.2.3 Horizon Heading .................................................................5-31
5.6.2.4 Airport Signs ....................................................................... 5-31
MFD
Sec 3
5.6.2.5 Runway Depiction ............................................................... 5-32
5.6.2.6 Traffic .................................................................................. 5-33
Sec 4
Hazard
5.6.2.7 Obstacles ............................................................................ 5-34
Avoidance
5.6.2.8 Field of View .......................................................................5-35
5.6.2.9 Unusual Attitudes ................................................................ 5-37
6 Annunciations and Alerts .....................................................................6-1
Sec 5
Features
Additional
6.1 Alerts ...................................................................................................6-1
6.2 System Status .......................................................................................6-7
7 Symbols ................................................................................................7-1
Sec 6
Annun.
& Alerts
7.1 Map Page Symbols ................................................................................7-1
7.2 SafeTaxi
7.3 Traffic Symbols ...................................................................................... 7-2
Sec 7
Symbols
7.4 Terrain Obstacle Symbols .......................................................................7-3
™ Symbols ............................................................................. 7-2
7.5 Basemap Symbols ................................................................................. 7-4
7.6 Map Tool Bar Symbols ........................................................................... 7-4
Sec 8
7.7 XM Weather Tool Bar Symbols ............................................................... 7-5
GlossaryAppendix A
7.8 Miscellaneous Symbols ..........................................................................7-6
8 Glossary ...............................................................................................8-1
Index
Appendix B
xii
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
Appendix A ................................................................................................. A-1
SD Card Use and Databases ..........................................................................A-1
Jeppesen Databases ...............................................................................A-1
Updating the Jeppesen navigation database ...........................................A-1
Garmin Databases ..................................................................................A-2
Updating Garmin databases ...................................................................A-3
Index ........................................................................................................... B-1
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Garmin G500H Pilot’s Guide
Symbols
Glossary Appendix A
Index
xiii190-01150-02 Rev. B
Sec 7
Sec 8
Appendix B
Foreword
Sec 1
System
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
Sec 6
Annun.
& Alerts
This page intentionally left blank
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Index
Appendix B
xiv
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
1 SYSTEM OVERVIEW
1.1 System Description
Foreword
This section provides an overview of the G500H Avionics Display System.
The G500H system is an integrated display system that presents primary flight
System
instrumentation, navigation, and a moving map to the pilot through large-format
displays.
In normal operating mode, the Primary Flight Display (PFD) presents
PFD
graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical
speed), replacing the traditional flight instrument cluster. The Multi-Function
Display (MFD) normally displays a full-color moving map with navigation
MFD
information.
GMU 44 Magnetometer
GRS 77H AHRS
GPS Navigator(s)
GDU 620
Optional Interfaces
Temperature Probe
GDC 74H Air Data Computer
Avoidance
Features
& Alerts
Symbols
Sec 1
Sec 2
Sec 3
Hazard
Sec 4
Additional
Sec 5
Annun.
Sec 6
Sec 7
Audio Panel
GDL 69/69A
Traffic
GTX330/330D
SL 30
Figure 1-1 G500H System (LRU Configuration)
The system consists of the following Line Replaceable Units (LRUs):
• GDU 620 Primary Flight Display (PFD) and Multi Function Display
(MFD)
• GDC 74H Air Data Computer (ADC)
• GRS 77H Attitude and Heading Reference System (AHRS)
• GNS 480, CNX80, GNS 400W series, or GNS 500W series GPS
Navigator
Garmin G500H Pilot’s Guide
1-1190-01150-02 Rev. B
Glossary Appendix A
Sec 8
Appendix B
Index
• Temperature Probe (such as the GTP 59)
• GMU 44 Magnetometer
• GTX 330/330D TIS-B Traffic (optional)
Foreword
• GDL 69A Satellite Data Link Receiver (optional)
• SL30 NavCom (optional)
Sec 1
System
• ADF (optional)
• GTS 800 Series Traffic (optional): (Similar functionality available in units
PFD
Sec 2
from third party providers)
• Audio Panel (optional)
1.1.1 Line Replaceable Units (LRU)
MFD
Sec 3
This guide covers the operation of the GDU 620 as integrated in the G500H
system. The G500H Avionics Display System is an advanced technology avionics
suite designed to replace the traditional flight instrument cluster. The system
Sec 4
Hazard
Avoidance
combines primary flight instrumentation, navigational information, and a
moving map all displayed on dual 6.5 inch color screens. The G500H system is
composed of sub-units or Line Replaceable Units (LRUs). LRUs have a modular
Sec 5
Features
Additional
design, which greatly eases troubleshooting and maintenance of the G500H
system. A failure or problem can be isolated to a particular LRU, which can
be replaced quickly and easily. Each LRU has a particular function, or set of
Sec 6
Annun.
& Alerts
functions, that contributes to the system’s operation.
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Index
Appendix B
1-2
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
1.1.2 GDU 620
The GDU 620 has dual VGA (640 x 480 pixels) 6.5 inch LCD displays. The
right side of the GDU is a PFD and the left side is the MFD. In some models or
installations, the PFD and MFD and their controls are switched to the other side.
The MFD shows a moving map, flight plan, weather, and more. The PFD shows
primary flight information, in place of traditional pitot-static and gyroscopic
systems and also provides an HSI for navigation.
Figure 1-2 GDU 620 PFD and MFD
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
1.1.3 GDC 74H
The GDC 74H Air Data Computer (ADC) compiles information from the
pitot/static system and an Outside Air Temperature (OAT) sensor. The GDC 74H
provides pressure altitude, airspeed, vertical speed, and OAT information to the
G500H system. The GDC 74H communicates with the GDU 620 and GRS 77H
using an ARINC 429 digital interface.
Figure 1-3 GDC 74H Air Data Computer
Garmin G500H Pilot’s Guide
1-3190-01150-02 Rev. B
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
1.1.4 GRS 77H
The GRS 77H is an Attitude and Heading Reference System (AHRS) unit that
provides aircraft attitude information to the G500H display. The unit contains
Foreword
advanced accelerometers and rate sensors. In addition, the GRS 77H interfaces
with both the GDC 74H Air Data Computer and the GMU 44 magnetometer.
The GRS 77H also utilizes GPS data forwarded from the GDU 620. Actual
Sec 1
System
attitude and heading information is sent to the GDU 620 using an ARINC 429
digital interface.
PFD
Sec 2
MFD
Sec 3
Figure 1-4 GRS 77H AHRS
Sec 4
Hazard
The IGRF (International Geomagnetic Reference Field) model is contained
Avoidance
in the GRS 77H and is only updated once every five years. The IGRF model
is part of the Navigation Database. At system power-up, the IGRF models in
Sec 5
the GRS 77H and in the Navigation Database are compared, and if the IGRF
Features
Additional
model in the GRS 77H is out of date, the user is prompted to update the IGRF
model in the GRS 77H. The prompt will appear after the G500H splash screen
is acknowledged on the MFD.
Sec 6
Annun.
& Alerts
1.1.5 GMU 44
The GMU 44 magnetometer senses the earth’s magnetic field. Data is sent
Sec 7
Symbols
to the GRS 77H AHRS for processing to determine aircraft magnetic heading.
This unit receives power directly from the GRS 77H and communicates with the
GRS 77H using a RS-485 digital interface.
Sec 8
GlossaryAppendix A
Figure 1-5 GMU 44 Magnetometer
Index
Appendix B
1-4
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
1.1.6 GTX 330/330D (Optional)
Foreword
Figure 1-6 GTX 330/330D Mode S Transponder
The GTX 330/330D is a solid-state transponder that provides Modes A, C,
and S functions. The transponder provides traffic information to the display
through an ARINC 429 digital interface.
NOTE: GTX 33/33D can also be used to display traffic information on the
GDU 620.
1.1.7 GTP 59
A temperature probe provides Outside Air Temperature (OAT) data to the
GDC 74H. The GTP 59 is an example of an appropriate temperature probe.
System
PFD
MFD
Avoidance
Features
Sec 1
Sec 2
Sec 3
Hazard
Sec 4
Additional
Sec 5
Figure 1-7 GTP 59 Temperature Probe
1.1.8 GSR 56
The GSR 56 supports the Position Reporting system which collects system
variables and transmits them over the Iridium® Satellite Network at a given
interval.
Garmin G500H Pilot’s Guide
1-5190-01150-02 Rev. B
& Alerts
Annun.
Sec 6
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
1.1.9 GDL 69/69A (Optional)
The GDL 69/69A is an XM Satellite Radio Data Link Receiver that receives
broadcast weather data. The GDL 69A is the same as the GDL 69 with the
Foreword
addition of an XM Satellite Radio audio entertainment receiver. Weather data
and control of audio channel and volume is displayed on the MFD, via a HighSpeed Data Bus (HSDB) Ethernet connection. The GDL 69A is also interfaced
Sec 1
System
to an audio panel for distribution of the audio signal. A subscription to the XM
Satellite Radio service is required to enable the GDL 69/69A capability.
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
1.1.10 Garmin Navigator Interface
The G500H system requires connection to at least one external Garmin
WAAS GPS navigator, such as the 400W/500W series or GNS 480.
Sec 6
Annun.
& Alerts
Figure 1-8 GDL 69/69A XM Satellite Radio Data Link Receiver
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Index
Appendix B
1-6
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
1.1.11 Attitude Heading Reference System (AHRS)
available
available
unavailable
unavailable
available
unavailable
unavailable
available
l
e
e
b
Airspeed Data
e
e
Magnetometer
unavailable
available
l
GPS
AHRS Normal
Operation
AHRS no-
Mag Mode
AHRS no-Mag/
no-Air Mode
Heading Invalid
AHRS
no-GPS
Mode
Attitude/Heading Invalid
NOTE: Aggressive maneuvering while AHRS is not operating in normal
mode may degrade AHRS accuracy.
Attitude and heading information is displayed on the PFD when the AHRS
receives appropriate combinations of information from the external sensor
inputs.
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
message advisory alerts (refer to Section 6 for specific AHRS alert information).
Any failure of the internal AHRS inertial sensors results in loss of attitude and
heading information (indicated by red “X” flags over the corresponding flight
instruments).
from one of the inputs fails, the AHRS uses the remaining GPS input and an
alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS
will continue to provide attitude and heading information to the PFD as long as
magnetometer and airspeed data are available and valid.
information and GPS Track information is used; however, the heading output
Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by
Figure 1-9 AHRS Operation
A maximum of two GPS inputs are provided to the AHRS. If GPS information
If the magnetometer input fails, the AHRS continues to output valid attitude
Garmin G500H Pilot’s Guide
Symbols
Glossary Appendix A
Index
1-7190-01150-02 Rev. B
Sec 7
Sec 8
Appendix B
on the PFD is flagged as invalid with a red “X,” “TRK” in magenta is annunciated
to the right of the Track value, and the Track value color is changed from white
to magenta.
Foreword
NOTE: In this case the magnetic standby compass and GPS ground track
can be used to keep the aircraft on the desired heading.
Sec 1
System
Failure of the air data input has no effect on the AHRS output while AHRS is
receiving valid GPS information. Invalid or unavailable airspeed data in addition
to complete GPS failure results in loss of all attitude and heading information.
PFD
Sec 2
1.1.12 Secure Data Cards
The G500H System uses Secure Digital (SD) cards to load and store various
MFD
Sec 3
types of data. For basic flight operations, SD cards are required for Terrain,
Obstacle, FliteChart, SafeTaxi, and ChartView database storage as well as
Jeppesen aviation and ChartView database updates. The Navigation Database
update card is inserted in the upper SD card slot for database updates and then
Sec 4
Hazard
Avoidance
removed. Other database cards are normally located in the lower SD card slot.
NOTE: Ensure the GDU 620 is powered off before inserting or removing
Sec 5
Features
Additional
an SD card.
NOTE: Refer to A-1 for instructions on updating the aviation database.
Sec 6
Annun.
& Alerts
Inserting an SD Card
1) Insert the SD card in the SD card slot (the front of the card should be flush with
Sec 7
the face of the display bezel).
Symbols
2) To eject the card, gently press on the SD card to release the spring latch.
Sec 8
GlossaryAppendix A
Index
Appendix B
1-8
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
1.1.13 Pilot Controls
The GDU 620 controls have been designed to simplify operation of the
system and minimize workload and the time required to access sophisticated
functionality. Controls are located on the PFD and MFD bezels and are comprised
of a PFD knob, MFD dual concentric knobs, bezel keys, and soft keys.
1.1.13.1 PFD Knob
Turning the PFD knob adjusts the values for the mode selected by the PFD
bezel keys, such as, Heading (HDG), Course (CRS), Altitude (ALT), Vertical
Speed (V/S), and Barometric Setting (BARO). The values are shown in a window
to the left of the HSI. Pressing the PFD knob reverts to the default value of the
selected mode.
Heading
Mode
Figure 1-10 Selection Modes Adjusted with the PFD Knob
NOTE: After 10 seconds of inactivity in another mode, the PFD knob
selected mode will revert to Heading mode.
Course
Mode
Altitude
Mode
Vertical Speed
Mode
Barometer
Mode
Foreword
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
1. Press the desired PFD mode selection key (HDG, CRS, A LT, V/S, or BARO). A
window will be displayed near the upper right corner of the HSI showing the
current value for that mode.
2. Turn the PFD knob to select the desired value.
Garmin G500H Pilot’s Guide
1-9190-01150-02 Rev. B
Symbols
Sec 7
Glossary Appendix A
Sec 8
Appendix B
Index
1.1.13.2 PFD Bezel Keys
Heading (HDG)
Selects Heading Select mode. Pressing the PFD knob in Heading mode will
Foreword
center the Heading Bug on the current Heading. This is the default mode for
the PFD knob. If the Heading is invalid, the PFD knob will revert to Course
Sec 1
mode. Set the heading on the HSI by turning the PFD knob after pressing
System
the HDG key.
Course (CRS)
PFD
Sec 2
Selects Course Select mode. Pressing the PFD knob in Course mode will
center the CDI for a VOR or OBS mode course.
Altimeter (ALT)
MFD
Sec 3
Selects Altitude Select mode. Pressing the PFD knob in Altimeter mode will
enter the current altitude in the Altitude Select window. Set the Altitude Bug
Sec 4
Sec 5
by turning the PFD knob after pressing the ALT key.
Hazard
Avoidance
Features
Additional
Altitude Select Window
Sec 6
Annun.
Sec 7
Sec 8
Appendix B
& Alerts
Symbols
GlossaryAppendix A
Index
1-10
Altitude Bug
Current Altitude
Barometric Setting
Figure 1-11 Pressing PFD Knob Sets Altitude Select to Current Altitude
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
Vertical Speed (V/S)
Selects Vertical Speed (V/S) mode. Pressing the PFD knob in V/S mode will
synchronize the bug to the current vertical speed.
Foreword
System
Sec 1
Vertical Speed Bug
Current Vertical Speed
PFD
MFD
Avoidance
Vertical Speed Bug Setting
Figure 1-12 Pressing V/S Knob Sets Vertical Speed Bug to Current Vertical Speed
Barometer (BARO)
Features
Selects Barometric Setting Select mode. Pressing the PFD knob in Baro mode
will enter the standard pressure (29.92 in) value.
1.1.13.3 PFD Soft Keys
& Alerts
The soft keys are located along the bottoms of the displays below the soft
key labels. The soft key labels shown depend on the soft key level or page being
Symbols
displayed. The soft keys can be used to select the appropriate soft key function.
Soft Key Labels
Soft Keys
Glossary Appendix A
Sec 2
Sec 3
Hazard
Sec 4
Additional
Sec 5
Annun.
Sec 6
Sec 7
Sec 8
Figure 1-13 PFD Soft Key Layout
When a soft key is selected, its color changes to black text on gray background
and remains this way until it is turned off, at which time it reverts to white text
on black background. When a soft key function is disabled, the soft key label
is subdued (dimmed). Soft keys revert to the previous level after 45 seconds of
inactivity.
Garmin G500H Pilot’s Guide
1-11190-01150-02 Rev. B
Appendix B
Index
Foreword
Sec 1
System
PFD
Sec 2
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
CDI
The CDI soft key toggles between the selection of GPS or VOR/LOC as the
active navigation source. The GDU CDI soft key will change the source in
the connected navigator and making a source change in the navigator will be
reflected in the GDU 620.
1-2
The 1-2 soft key toggles between the available receivers for selected navigation
source (i.e. GPS1 and GPS2 or VOR/LOC1 and VOR/LOC2). This soft key
will only be present if the system is configured for a second GPS or VOR/
LOC.
ATT SYNC
Pressing the ATT SYNC soft key will synchronize the aircraft symbol on the
PFD to the horizon line during level flight. The ATT SYNC soft key will not
be available for selection until the aircraft is near a level pitch attitude.
PFD
Pressing the PFD soft key displays the BRG1, BRG2, and BACK soft keys.
The BRG2 soft key will only be present if the system is configured for a
second GPS or VOR/LOC receiver.
Sec 6
Annun.
Sec 7
Sec 8
Appendix B
BRG1
The BRG1 soft key cycles through the available bearing 1 indicator modes
& Alerts
(NAV1, GPS1, ADF, or None).
BRG2
Symbols
The BRG2 soft key cycles through the available bearing 2 indicator modes
(NAV2, GPS2, ADF, or None). This soft key will only be present if the system
is configured for a second GPS or VOR/LOC.
GlossaryAppendix A
SYN VIS
The SYN VIS soft key is available if Synthetic Vision Technology™ is installed.
It enables Synthetic Vision and displays the associated soft keys.
SYN TERR
The SYN TERR soft key is available if Synthetic Vision Technology™ is
Index
installed and enables synthetic terrain depiction.
1-12
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
HRZN HDG
The HRZN HDG soft key is available if Synthetic Vision Technology™ is
Foreword
installed. Pressing this key enables horizon heading marks and digits.
APTSIGNS
The APTSIGNS soft key is available if Synthetic Vision Technology™
is installed and enables airport sign posts for airports. Heliports are not
shown.
BACK
The BACK soft key returns to the pages default soft key options.
1.1.13.4 MFD Knobs
The MFD knobs are for navigating and selecting information on the MFD
pages. More details are provided in the MFD section.
Small (Inner) MFD Knob
Selects a specific page within a page group. Pressing the small MFD knob
turns the selection cursor ON and OFF. When the cursor is ON, data may be
entered in the applicable window by turning the small and large MFD knobs.
In this case, the large MFD knob moves the cursor on the page and the small
MFD knob selects individual characters or values for the highlighted cursor
location.
Large (Outer) MFD Knob
Selects the MFD page group. When the cursor is ON, the large MFD knob
moves the cursor to highlight available fields.
System
Sec 1
Sec 2
PFD
Sec 3
MFD
Avoidance
Hazard
Sec 4
Additional
Features
Sec 5
& Alerts
Annun.
Sec 6
Symbols
Sec 7
1.1.13.5 MFD Bezel Keys
Range (RNG)
Pressing the Range arrow keys changes the range on the Map pages. The Up
arrow zooms out. The Down arrow zooms in. The keys also aid in scrolling
up and down text pages.
Menu
Displays a context-sensitive list of options. This list allows the user to access
additional features or make setting changes that relate to particular pages.
Garmin G500H Pilot’s Guide
1-13190-01150-02 Rev. B
Glossary Appendix A
Sec 8
Appendix B
Index
Enter (ENT)
Validates or confirms a menu selection or data entry.
Clear (CLR)
Foreword
Erases information, cancels entries, or removes page menus. Pressing and
holding the CLR key displays the Navigation Map 1 page.
Sec 1
System
1.1.13.6 MFD Soft Keys
MFD functions indicated by the soft key labels vary depending on the page
selected and are located at the bottom of the MFD display. Press the soft key
PFD
Sec 2
located directly below the soft key label. To select the function indicated on the
soft key label, press the soft key directly below the label.
MFD
Sec 3
Sec 4
Hazard
Avoidance
Sec 5
Features
Additional
Sec 6
Annun.
& Alerts
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Selected Soft Key
Unselected Soft Keys
Figure 1-14 MFD Soft Key Layout
Soft Key Labels
Soft Keys
Appendix B
Index
1-14
Garmin G500H Pilot’s Guide
190-01150-02 Rev. B
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