Garmin G500 User manual

G500
Cockpit
Reference Guide

© 2009 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 3.00, or later. Some differences in operation
may be observed when comparing the information in this manual to later software versions.
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October 2009 Printed in the U.S.A.

i
G500 Cockpit Reference Guide
190-01102-03 Rev C
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from
the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components
that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts
and labor, provided that the customer shall be responsible for any transportation cost. This warranty does
not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER
WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER
ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR
OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL
DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR
FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential
damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the
purchase price, at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR
ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local GarminAuthorized 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.

ii G500 Cockpit Reference Guide 190-01102-03 Rev C
WARNINGS, CAUTIONS, AND NOTES
WARNINGS, CAUTIONS, AND NOTES
Warnings, Cautions, & Notes
WARNING: Navigation and terrain separation must NOT be predicated
upon the use of the terrain function.The GDU 620 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 warning 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 GDU 620 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 GDU 620. It is thus the responsibility
of the pilot to detect such an occurrence by means of cross-checking with
all redundant or correlated information available in the cockpit.
WARNING: 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 74A
Air Data Computer, or other pressure altimeters in aircraft. GPS altitude
should never be used for vertical navigation.Always use pressure altitude
displayed by the GDU 620 PFD or other pressure altimeters in aircraft.
WARNING: Do not use outdated database information. Databases used
in the G500 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.

iii
G500 Cockpit Reference Guide
190-01102-03 Rev C
WARNINGS, CAUTIONS, AND NOTES
WARNINGS, CAUTIONS, AND NOTES
WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the GDU 620 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, GDU 620 operational procedures must be
learned on the ground.
WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G500 Pilot’s Guide. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully
compare indications from the GDU 620 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: Never use the G500 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 invalidateAHRS
attitude provided to the GDU 620. Exceeding 450 KIAS may invalidate ADC
information provided to the GDU 620.

iv G500 Cockpit Reference Guide 190-01102-03 Rev C
WARNINGS, CAUTIONS, AND NOTES
WARNINGS, CAUTIONS, AND NOTES
WARNING: Because of anomalies in the earth’s magnetic field, operating
the G500 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 south of 55° South latitude between
longitude 120° East and 165° East.
WARNING: Do not use Terrain-SVT information for primary terrain
avoidance. Terrain-SVT 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 GDU 620 utilize
GPS as a precision electronic NAVigation AID (NAVAID).Therefore, as with
all NAVAIDs, information presented by the GDU 620 can be misused or
misinterpreted and therefore, become unsafe.
CAUTION: The Garmin GDU 620 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
pilot’s authority to operate this device under FAA/FCC regulations.
CAUTION: The GDU 620 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.

v
G500 Cockpit Reference Guide
190-01102-03 Rev C
WARNINGS, CAUTIONS, AND NOTES
WARNINGS, CAUTIONS, AND NOTES
NOTE: All visual depictions contained within this document, including
screen images of the GDU 620 bezel displays, are subject to change and
may not reflect the most current G500 system. Depictions of equipment
may differ slightly from the actual equipment.
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: 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: Terrain-SVT is standard when the Synthetic Vision Technology™
(SVT) option is installed. The TAWS option will take precedence over
Terrain-SVT.

vi G500 Cockpit Reference Guide 190-01102-03 Rev C
Record of Revisions
Part Number Revision Date Page
Range Description
190-01102-03
190-01102-03
190-01102-03
A
B
C
5/28/09
6/18/09
10/26/09
All
Cover
55
Production Release
Updated logo to meet
guidelines and added Garmin
to SVT™.
Updated subscription
information for FliteCharts
and ChartView.

vii
G500 Cockpit Reference Guide
190-01102-03 Rev C
TABLE OF CONTENTS
TABLE OF CONTENTS
Contents
Warnings, Cautions, & Notes ............................................................................ ii
Introduction...................................................................................................... 1
Primary Flight Display (PFD)............................................................................. 2
Airspeed Tape.............................................................................................................................. 4
Altitude Tape............................................................................................................................... 5
Barometric Pressure..................................................................................................................... 5
Barometric Minimums Bug........................................................................................................... 6
Altitude Bug................................................................................................................................ 7
Wind Vectors............................................................................................................................... 8
Vertical Speed (V/S) ..................................................................................................................... 8
Vertical Deviation Indicator (VDI) ................................................................................................. 9
Outside Air Temperature (OAT)..................................................................................................... 9
Attitude Indicator ...................................................................................................................... 10
Horizontal Situation Indicator (HSI): Aircraft Heading .................................................................. 11
Adjusting the Course Pointer ..................................................................................................... 12
HSI Bearing Pointers .................................................................................................................. 12
Autopilot (AP)................................................................................................. 15
Heading .................................................................................................................................... 15
Autopilot Test............................................................................................................................ 15
Altitude Capture (Optional Interface) ......................................................................................... 16
Autopilot Navigation ................................................................................................................. 16
Autopilot Operation with the GDU 620 Emulating GPSS............................................................. 17
Additional Features........................................................................................ 18
Garmin Synthetic Vision Technology™(Optional)......................................................................... 18
Displaying Garmin SVT™Terrain................................................................................................. 19
Displaying Heading on the Horizon ............................................................................................ 19
Displaying Airport Signs............................................................................................................. 19
Multi-Function Display (MFD)......................................................................... 20
Page Navigation - Moving Between Pages ................................................................................. 21
Changing Settings within a Page................................................................................................ 21
Default Map Page...................................................................................................................... 21
MFD Soft Key Map..................................................................................................................... 22
Map Group ..................................................................................................... 23
Navigation Map 1 and Navigation Map 2 Pages......................................................................... 23
Decluttering (DCLTR) the Map Pages.......................................................................................... 24
Traffic Map Page (Optional) ....................................................................................................... 27
Terrain Page .............................................................................................................................. 31
Terrain Pop-Up Alerts................................................................................................................. 33
WX Group ....................................................................................................... 34
WX Data Link Map Pages .......................................................................................................... 34

viii G500 Cockpit Reference Guide 190-01102-03 Rev C
TABLE OF CONTENTS
TABLE OF CONTENTS
Customizing the Weather Map................................................................................................... 34
Displaying Surface Data and Winds Aloft.................................................................................... 36
Weather Radar (Optional) .............................................................................. 37
Weather Radar Map Page.......................................................................................................... 37
Airborne Color Weather Radar...................................................................................................38
Aux Group ...................................................................................................... 41
System Setup Page .................................................................................................................... 41
XM®Information Page (Optional) .............................................................................................. 46
XM®Radio Page (Optional) ....................................................................................................... 47
System Status Page ................................................................................................................... 49
Flight Plan Group ........................................................................................... 50
Active Flight Plan Page .............................................................................................................. 50
Viewing Your Active Flight Plan.................................................................................................. 50
Waypoint Information Page........................................................................................................ 51
Charts Page (Optional) .............................................................................................................. 52
Change Day/Night View............................................................................................................. 52
Viewing Charts and Panning...................................................................................................... 52
Viewing NOTAMs ...................................................................................................................... 53
Selecting a Chart....................................................................................................................... 53
Selecting Other Charts............................................................................................................... 54
Chart Information...................................................................................................................... 55
Alerts.............................................................................................................. 56
On Screen Alerts........................................................................................................................ 56
Terrain-SVT™Alerts ................................................................................................................... 58
Symbols .......................................................................................................... 59
Map Page Symbols .................................................................................................................... 59
SafeTaxi®Symbols ..................................................................................................................... 60
Traffic Symbols .......................................................................................................................... 60
Terrain Obstacle Symbols ........................................................................................................... 61
Map Toolbar Symbols ................................................................................................................ 61
XM®Weather Toolbar Symbols................................................................................................... 62
Miscellaneous Symbols .............................................................................................................. 63

1
G500 Cockpit Reference Guide
190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Introduction
This reference guide covers the operation of the GDU 620 as integrated in the
G500 system. The G500 Avionics Display System is an advanced technology
avionics suite designed to replace the traditional flight instrument cluster. The
system combines primary flight instrumentation, navigational information, and
a moving map all displayed on dual 6.5 inch color screens. The G500 system is
composed of sub-units or Line Replaceable Units (LRUs). LRUs have a modular
design and can be installed directly behind the instrument panel or in a separate
avionics bay if desired. This design greatly eases troubleshooting and maintenance
of the G500 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 functions, that contributes to the system’s operation. For more details
on the G500 system, refer to the G500 Pilot’s Guide, P/N 190-01102-02 Rev. A
or later.
PFD/MFD

2 G500 Cockpit Reference Guide 190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Primary Flight Display (PFD)
1
2
4
5
6
7
8
3
910 11 12
14
15
13
16
17
18
Primary Flight Display (PFD)

3
G500 Cockpit Reference Guide
190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
1NAV Status Bar: Displays which GPS is selected as the Active Source, Active Waypoint
(WPT), Distance to Waypoint (DIS), Desired Track (DTK) and Current Track (TRK).
2Airspeed Tape: Displays Groundspeed (GS), Airspeed Trend, Current Airspeed,
and True Airspeed (TAS).
3Wind Vector: Displays direction and speed of wind.
4Heading Select Key: Press HDG and turn PFD knob to set heading bug.
5Course Select Key: Press CRS and turn PFD knob to set the course of the
selected source (VOR1, VOR2, GPS1, or GPS2).
6Altitude Select Key: Press ALT and turn PFD knob to set altimeter bug.
7V/S (Vertical Speed) Select Key: Press V/S and turn PFD knob to set V/S bug.
8Barometer Select Key: Press BARO and turn PFD knob to change barometric
setting.
9Outside Air Temperature (OAT): Displays the current outside air temperature.
10 PFD Knob: Turn PFD knob to change bug settings, Heading Bug, Course,
Altitude Bug, V/S Bug, and Barometer setting.
11 Soft Keys: Used to select available options on PFD or MFD.
12 SD Card Slots, Upper and Lower: The upper slot is used for updating databases
or software, the lower slot is for the database card.
13
Soft Key Labels: Located on the bottom screen of the PFD and MFD. Selection
is done by pressing the corresponding soft key. Soft keys that are available
have the labels shown as white text on a black background. Soft keys that are
selected have the labels shown as black text on a gray background. Soft keys
that are unavailable have the labels shown as gray text on a black background.
14 Horizontal Situation Indicator (HSI): Displays the Selected Heading Box, Current
Heading, Turn Rate Markings, and Heading Trend.
15 Vertical Speed Tape: Displays Vertical Speed and the Vertical Speed Bug
16 Barometric (BARO) Setting: Displays the current setting of barometric pressure.
17
Roll Pointer and Slip/Skid Indicator: The slip/skid indicator is the bar beneath the
roll pointer. The indicator moves with the roll pointer and laterally away from the
pointer to indicate lateral acceleration (slip/skid).
18 Altitude Tape: Displays Current Altitude, Altitude Trend, Altitude Bug, Altitude
Minimums Bug, and BARO setting.

4 G500 Cockpit Reference Guide 190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Airspeed Tape
The upper left portion of the PFD display provides Groundspeed, Airspeed
Trend, Current Airspeed, and True Airspeed information. Current Airspeed is
normally shown in white on the black pointer. The Trend Indicator (magenta line)
indicates what the airspeed will be in six seconds, if the current rate of acceleration
is maintained. If the current acceleration will cause the airspeed to exceed V
NE in
six seconds, the airspeed is displayed in yellow. If the current airspeed exceeds
V NE , the pointer changes to red with white text.
V NE
V N0
V FE
V S0
V S1
Groundspeed
Trend Indicator
True Airspeed
Current
Airspeed
Typical Airspeed Tape Markings Airspeed Tape
Overspeed
Overspeed Indication Additional Reference Markings
VYSE
VMCA
VLE

5
G500 Cockpit Reference Guide
190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Altitude Tape
The upper right portion of the PFD displays the Altitude Bug setting, Current
Altitude, Altitude Trend, Altitude Minimums Bug, and the current BARO Setting.
The Altitude Trend indicates what the altitude will be in six seconds if the current
vertical speed is maintained.
Altitude Bug Setting
Altitude Trend
BARO Setting
Current Altitude
Altitude Tape
Altitude Bug
Altitude Minimums Bug
Barometric Pressure
The Barometric Pressure (BARO setting) is displayed at the bottom of the
altitude tape. To change the BARO setting, press the BARO key and turn the
PFD knob to the desired pressure. To select standard pressure (29.92 IN ), press
the PFD knob.

6 G500 Cockpit Reference Guide 190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Barometric Minimums Bug
For altitude awareness, a barometric Altitude Minimums Bug commonly referred
to as the Minimums Bug, can be set. When active and within 2500 feet of the
selected minimums altitude, the minimums bug setting is displayed to the bottom
left of the altimeter. When set, a bug appears parked at the bottom of the altitude
tape and moves up the tape as the set altitude comes into view.
When the aircraft altitude descends to within 2500 feet of the selected•
altitude minimums setting, the BARO MIN box appears with the
altitude value in cyan text. Once in range, the Minimums Bug appears
in cyan on the altitude tape.
A portion of the Minimums Bug will
be displayed at the bottom of the altitude tape if the selected altitude
minimums bug is off of the tape.
When the aircraft is within 100 feet of the selected altitude minimums•
setting, the bug and the altitude text turn white.
Once the aircraft reaches the selected altitude minimums setting, the•
bug and the altitude text turn yellow and the aural alert, “Minimums,
minimums” is heard one time.
Minimums
Bug
Minimums
Box
Bug and text are
cyan within 2500 ft
Bug and text are
white within 100 ft
Bug and text
are yellow when
altitude Reached
Minimums Annunciations
Alerting is inhibited while the aircraft is on the ground and also, if a value has
been set for altitude alerting, until the aircraft reaches 150 feet above the setting
for the alert.

7
G500 Cockpit Reference Guide
190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
To set the altitude for the Minimums Bug:
While viewing the Active Flight Plan page of the FPL Group, press the small1)
MFD knob to activate the cursor.
Turn the large2) MFD knob to the ALTITUDE portion of the MINIMUMS section.
Turn the small3) MFD knob to enter the desired altitude. Press the ENT key to
confirm selection.
When finished, press the small4) MFD knob to exit the MINIMUMS box.
NOTE: If you highlight the Altitude Field in the MINIMUMS section on the
FPL page and press the CLR key, it will clear the entry and the minimums
functionality will be turned off.
Altitude Bug
The Altitude Bug is displayed on the Altitude Tape at the selected altitude bug
setting. A portion of the Altitude Bug will be displayed at the top or bottom of
the altitude tape if the selected altitude bug is off of the tape.
Altitude Bug
Altitude Bug
Altitude Bug
Setting
The Altitude Bug provides visual and aural altitude alerting. Aural alerting
occurs within 200 feet of the Altitude Bug setting or when deviating beyond 200
feet of the bug.
Within 1000 ft Within 200 ft Deviation of
+/- 200ft
Altitude Bug Indications

8 G500 Cockpit Reference Guide 190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Wind Vectors
The PFD will display a Wind Vector Field to the left of the HSI when configured
by the user. There are four different styles of wind vector displays available. Refer
to the System Setup page in the AUX Group section of this guide for instructions
on selecting wind vector style. Wind Vectors can only be calculated when the
aircraft is in the air.
Wind Vector
Field
Wind Vector Display
Vertical Speed (V/S)
The Vertical Speed Tape and Vertical Speed Bug are displayed below the
Altitude Tape.
Current Vertical Speed
Vertical Speed Bug Setting
Vertical Speed
Vertical Speed Bug

9
G500 Cockpit Reference Guide
190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Vertical Deviation Indicator (VDI)
The Vertical Deviation Indicator is displayed for GPS and ILS approaches
with vertical guidance. The GPS approach glidepath is shown in magenta
(G and indicator), while the ILS approach glideslope is shown in green
(G and indicator.)
GPS Approach
Vertical Deviation Source
Vertical Deviation Indicator
ILS Approach
Outside Air Temperature (OAT)
The Outside Air Temperature, as sensed from the temperature probe on the
aircraft, is displayed to the left of the HSI. This temperature is used in calculating
the true airspeed.

10 G500 Cockpit Reference Guide 190-01102-03 Rev C
PRIMARY FLIGHT DISPLAY (PFD)
PRIMARY FLIGHT DISPLAY
Attitude Indicator
The standby mechanical Attitude Indicator in your aircraft is either a Ground
Pointer or a Roll Pointer configuration. The GDU 620 Attitude Indicator has been
configured in either a Ground Pointer or a Roll Pointer configuration to match
the configuration of your aircraft’s standby Attitude Indicator.
In an aircraft with an Attitude Indicator that has a Ground Pointer, the pointer
above the roll scale shifts with the roll or bank angle of the aircraft to keep the
Roll Scale Zero Pointer pointing towards the ground.
Roll Pointer Roll Scale Zero Pointer
Roll Scale
G500 Attitude Indicator with a Ground Pointer Configuration in a Left Turn
In an aircraft with an Attitude Indicator that has a Sky Pointer, the pointer
below the roll scale shifts with the roll or bank angle of the aircraft to keep the
Roll Pointer pointing towards the sky.
Roll Scale
Roll Scale Zero Pointer
Roll Pointer
G500 Attitude Indicator with a Sky Pointer Configuration in a Left Turn