This manual reflects the operation of system software version 7.00, or later. Some differences in operation
may be observed when comparing the information in this manual to later software versions.
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, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40
9RB, U.K. Tel. +44 (0) 870 850 1243 Fax +44 (0) 238 052 4004
Garmin Corporation, No. 68, Jangshu 2nd Road, Xizhi Dist., New Taipei City 221, Taiwan (R.O.C.)
Tel: 886.02.2642.9199 Fax: 886.02.2642.9099
www.garmin.com
At Garmin, we value your opinion. For comments about this guide, please e-mail:
Techpubs.Salem@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®, GDU™ 620 are trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are
registered trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the
express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; SkyWatch® is a registered trademark of L-3 Avionics
Systems; and SiriusXM® is a registered trademark of Sirius XM Radio, Inc.; Iridium® is a registered
trademark of Iridium Communications Inc.; Canadian radar data provided by Environment Canada; United
States radar data provided by NOAA; European radar data collected and provided by Meteo France.
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.
April 2015 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 products or services that are obtained and/or used in contravention of the laws of any country.
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, 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 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.
Online Auction Purchases: Products purchased through online auctions are not eligible for warranty
coverage. Online auction confirmations are not accepted for warranty verification. To obtain warranty
service, an original or copy of the sales receipt from the original retailer is required. Garmin 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 866.739.5687.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
i
WARNINGS, CAUTIONS, AND NOTES
Warnings, Cautions, & Notes
WARNING:
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:
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:
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.
Navigation and terrain separation must NOT be predicated
The displayed minimum safe altitudes (MSAs) are only advisory
The Garmin GDU 620 has a very high degree of functional
WARNINGS, CAUTIONS, AND NOTES
ii
WARNING:
above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the output from the GDC 74A/B
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:
in the G500 or G600 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.
The altitude calculated by GPS receivers is geometric height
Do not use outdated database information. Databases used
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
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:
Display is provided as an aid in visually acquiring traffic. Pilots must
Traffic information shown on the GDU 620 Multi-Function
maneuver the aircraft based only upon ATC guidance or positive visual
acquisition of conflicting traffic.
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.
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 G500/600 Pilot’s Guide. Thoroughly practice
basic operation prior to actual use. During flight operations, carefully
compare indications from the G500/600 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.
WARNINGS, CAUTIONS, AND NOTES
WARNING: Exceeding 200 deg/second in pitch or roll may invalidate AHRS
attitude provided to the GDU 620. Exceeding 450 KIAS may invalidate ADC
information provided to the GDU 620.
WARNING: Because of anomalies in the earth’s magnetic field, operating
the G500/600 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 85° East and 114° West. An area south of 55° South
latitude between longitude 120° East and 165° East.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
iii
WARNINGS, CAUTIONS, AND NOTES
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.
WARNINGS, CAUTIONS, AND NOTES
iv
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: 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.
NOTE: All visual depictions contained within this document, including
screen images of the GDU 620 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.
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
WARNINGS, CAUTIONS, AND NOTES
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-SVT is standard when the Synthetic Vision Technology™
(SVT) option is installed. The TAWS option will take precedence over TerrainSVT.
NOTE: Do not use SafeTaxi, FliteCharts, or Chartview functions as the
basis for ground maneuvering. SafeTaxi, FliteCharts, and Chartview
functions have not been qualified to be used as an airport moving map
display (AMMD). SafeTaxi, FliteCharts, and Chartview are intended
to improve pilot situational awareness during ground operations and
should only be used by the flight crew to orient themselves on the
airport surface.
WARNINGS, CAUTIONS, AND NOTES
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
v
Record of Revisions
Part Number RevisionDateDescription
190-00601-03A
B
6/12/08
6/1/09
Production release
Revision reflects functionality added with
SW version 3.00. Added SVT, TAWS-B,
Terrain Proximity, Wind Vectors, Minimums
Bug, GAD 43, and Weather Radar
information.
C
10/26/09
Updated subscription information for
FliteCharts and ChartView.
D
11/30/10
Added changes to reflect v4.00 and v5.00
software changes.
E
8/23/11
Added changes to reflect v6.00 software
changes.
F
10/23/12
Added changes to reflect v6.11 software
changes.
G
4/10/15
Added changes to reflect software
version 7.00. G500 and G600 CRG’s are
combined.
Temperature Display ...................................................................................................................................11
Flight Director Display .................................................................................................................................22
Vertical Speed Control ................................................................................................................................ 22
Customizing the Weather Map ....................................................................................................................44
Changing Forecast Time .............................................................................................................................. 46
Airborne Color Weather Radar ....................................................................................................................52
Aux Group ...................................................................................................... 55
External Video Page (Optional) .................................................................................................................... 55
System Setup Page .....................................................................................................................................56
XM® Information Page (Optional) ...............................................................................................................62
XM® Radio Page (Optional) ........................................................................................................................63
Position Reporting Page .............................................................................................................................. 65
System Status Page.....................................................................................................................................68
Flight Plan Group ........................................................................................... 69
Active Flight Plan Page ...............................................................................................................................69
Viewing Your Active Flight Plan ................................................................................................................... 69
Waypoint Information Page.........................................................................................................................70
Chart Information ....................................................................................................................................... 71
Selecting a Chart ........................................................................................................................................ 71
Selecting Other Charts ................................................................................................................................ 72
Viewing Charts and Panning .......................................................................................................................72
TABLE OF CONTENTS
Viewing Details of ChartView™ Charts .......................................................................................................73
On Screen Alerts ......................................................................................................................................... 75
This reference guide covers the operation of the GDU 620 as integrated in
the G500 and G600 Avionics Display Systems. The G500 and G600 Avionics
Display Systems are avionics suites that combine primary flight instrumentation,
navigational information, and a moving map all displayed on dual 6.5 inch
color screens. The G500 and G600 systems are 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 or
G600 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 and G600 systems, refer to the latest revision of the G500/600 Pilot’s Guide,
P/N 190-00601-02.
PRIMARY FLIGHT DISPLAY
PFD/MFD
NOTE: In some models or installations, the PFD and MFD and their controls
are switched to the other side.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
1
PRIMARY FLIGHT DISPLAY (PFD)
Primary Flight Display (PFD)
21
PRIMARY FLIGHT DISPLAY
1
2
3
4
5
6
7
8
9
1011
Airspeed Tape: Displays Groundspeed (GS), Airspeed Trend, Current Airspeed,
1
and True Airspeed (TAS). Markings dependent upon installation configuration.
22
Primary Flight Display (PFD)
20
19
18
17
16
15
14
13
12
2
Wind Vector: Displays direction and speed of wind.
3
Heading Select Key: Press HDG and turn PFD knob to set heading bug.
Course Select Key: Press CRS and turn PFD knob to set the course of the
4
selected source (VOR1, VOR2, GPS1, or GPS2).
5
Altitude Select Key: Press ALT and turn PFD knob to set altimeter bug.
6
V/S (Vertical Speed) Select Key: Press V/S and turn PFD knob to set V/S bug.
Barometer Select Key: Press BARO and turn PFD knob to change barometric
7
setting.
2
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Outside Air Temperature (SAT, TAT, or ISA): Displays the current outside air
8
temperature.
NAV Status Window: (NAV Style 2 Shown) Displays which GPS is selected as
the Active Source, Active Waypoint (WPT), and Distance to Waypoint (DIS).
9
NAV Style 1 (Not Shown) displays Active Source, WPT, DIS, Desired Track (DTK),
and Current Track (TRK) at top of screen.
Soft Keys: Used to select available options on PFD or MFD.
SD Card Slots, Upper and Lower: The lower slot is used for the supplemental
12
database card, including aviation database updates. The upper slot may be used
to update the internal aviation database.
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
13
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.
Horizontal Situation Indicator (HSI): Displays the Selected Heading Box, Current
14
Heading, Turn Rate Markings, and Heading Trend.
PRIMARY FLIGHT DISPLAY
15
Vertical Speed Tape: Displays Vertical Speed and the Vertical Speed Bug
16
Barometric (BARO) Setting: Displays the current setting of barometric pressure.
Radar Altimeter Display: Displays current height above ground from the radar
17
altimeter. Brown band in altitude tape represents the ground.
18
Fast/Slow Indicator: See your AFM for details on operation.
Roll Pointer and Slip/Skid Indicator: The slip/skid indicator is the bar beneath the
19
roll pointer. The indicator moves with the roll pointer and laterally away from the
pointer to indicate lateral acceleration (slip/skid).
Altitude Tape: Displays Current Altitude, Altitude Trend, Altitude Bug, Altitude or
20
Radar Altimeter Minimums Bug, and BARO setting.
21
Marker Beacon: Marker Beacon Indicator
22
Clock or Timer window.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
3
PRIMARY FLIGHT DISPLAY (PFD)
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 acceleration
is maintained. If the current acceleration will cause the airspeed to exceed Vne in
six seconds, the airspeed is displayed in yellow. If the current airspeed exceeds
Vne, the pointer changes to red with white text.
NOTE: Airspeed tape markings are dependent upon configuration at
the time of installation. Reference the AFM or POH or latest revision
of the G500/600 Pilot’s Guide for more details.
Groundspeed
Mmo/
Vmo/
Vne
Vno
Vfe
Vs0
PRIMARY FLIGHT DISPLAY
Typical Airspeed Tape Markings
Overspeed
Overspeed Indication
Vs1
Current
Airspeed
Airspeed Tape
Additional Reference Markings
Reference Speeds
Trend Indicator
True Airspeed
White triangle
(See AFM/POH)
V
YSE
V
Maximum speed
with landing gear
MCA
extended.
4
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
V-speeds (Glide, Vr, VX, and VY) default values are set during the installation
process, but can be changed and turned on/off from the System Setup page on the
first page of the Aux page group. When active (on), the V-speeds are displayed
at their respective locations to the right of the airspeed scale.
Glide Reference Marker
Vr Reference Marker
Vx Reference Marker
Vy Reference Marker
Reference Speeds
The labels for the reference markers may vary as configured during installation.
Reference Marker
V2 Reference Marker
V1 Reference Marker
Vr Reference Marker
PRIMARY FLIGHT DISPLAY
190-00601-03 Rev G
Alternate Reference Speeds
G500/600 Cockpit Reference Guide
5
PRIMARY FLIGHT DISPLAY (PFD)
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 Bug
Altitude Trend
Altitude Minimums Bug
BARO Setting
Altitude Tape
Current Altitude
PRIMARY FLIGHT DISPLAY
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 (29.92in, 1013 mb), press
the PFD knob. To return to the previous setting, press the PFD knob again.
6
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Minimums Bug (Barometric or Radar Altimeter)
For altitude awareness, an Altitude Minimums Bug commonly referred to as
the Minimums Bug, can be set. the source of data for minimums alerting can be
selected to either barometric altitude or radar altitude (if installed.) 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 minimums 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.
Bug and text
Bug and text are
cyan within 2500 ft
Bug and text are
white within 100 ft
are yellow when
altitude reached
PRIMARY FLIGHT DISPLAY
Minimums
Bug
Minimums
Box
Minimums Annunciations using BARO for Source
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.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
7
PRIMARY FLIGHT DISPLAY (PFD)
To set the altitude for the Minimums Bug:
1) While viewing the Active Flight Plan page of the FPL Group, press the small
MFD knob to activate the cursor and turn the large MFD knob to the Source
selection.
2) Turn the small MFD knob to select Off, BARO, or RAD ALT.
3) Turn the large MFD knob to the ALTITUDE portion of the MINIMUMS section.
4) Turn the small MFD knob to enter the desired altitude. Press the ENT key to
confirm selection.
5) When finished, press the small MFD knob to exit the MINIMUMS box.
The Minimums Bug can also be set from the Charts page of the FPL.
1) While viewing the Charts page of the FPL Group, press the MENU key and
select “Set Minimums” from the Options menu.
2) Turn the small MFD knob to select Off, BARO, or RAD ALT.
3) Press the ENT key to move to enter altitude. Turn the small MFD knob to
enter the desired altitude. Press the ENT key to confirm selection.
PRIMARY FLIGHT DISPLAY
Radar Altimeter Value
8
Minimums Annunciations using RAD ALT for Source
G500/600 Cockpit Reference Guide
Brown band represents
the ground.
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
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
Setting
Altitude Bug
PRIMARY FLIGHT DISPLAY
Altitude Bug
The Altitude Bug provides visual and aural altitude alerting. Aural alerting
occurs within 200 feet (or 1000 feet, as configured) 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
Fast/Slow Indication
The Fast/Slow indication from an external system may be optionally displayed
on the left side of the PFD. Refer to the Airplane Flight Manual for instructions
on using the Fast/Slow indications.
Pointer
Fast/Slow Scale
Fast/Slow Scale and Pointer
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
9
PRIMARY FLIGHT DISPLAY (PFD)
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. For aircraft with vertical speed operating limitations, red bands showing
Vertical Speed Maximum and Minimum ranges will be shown on the left side of
the Vertical Speed tape.
Vertical
Speed Bug
PRIMARY FLIGHT DISPLAY
10
Vertical Speed
G500/600 Cockpit Reference Guide
Vertical Speed
Current
Vertical Speed
Vertical Speed Bug
Setting
Maximum
Vertical Speed
Minimum
Vertical Speed Warning
Indication
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Vertical Deviation Indicator (VDI)
The Vertical Deviation Indicator is displayed for ILS and GPS 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.)
Vertical Deviation Source
Vertical Deviation Indicator
PRIMARY FLIGHT DISPLAY
GPS Approach
ILS Approach
Temperature Display
The outside air temperature is displayed to the left of the HSI. The air data
computer calculates the temperature based on temperature probe and pitot/
static inputs. The units (°C or °F) and temperature reference are selected on the
AUX – SYSTEM SETUP page. The temperature reference can be selected to one
of the following choices:
•
Static Air Temperature (SAT) – This is the calculated temperature of the
stationary (static) outside air. Conceptually, this is the temperature that
would be read on a thermometer floating stationary at the current location.
• Total Air Temperature (TAT) – This is the calculated temperature of the
outside air as it moves past the aircraft, including the rise in temperature
due to air compression and friction at the current airspeed.
• Difference from International Standard Atmosphere (ISA) – This is the
difference between SAT and standard (ISA) temperature at the current
altitude. This provides an indication of how much warmer/colder the
temperature is from a “standard” atmosphere.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
11
PRIMARY FLIGHT DISPLAY (PFD)
DME Indication
DME information is displayed in a window in the lower left corner of the PFD.
The distance to the station and the NAV source used are shown.
DME Information
DME Hold Annunciation
Selected DME
Set Hold for Selected DME
DME Indication
Clock/Timer
The Clock/Timer function displays a clock or timer window in the lower left
corner of the PFD.
Show/Hide Clock
Show/Hide Timer
Select Timer
Select Clock
Clock and Timer Functions
Start/StopTimerReset Timer
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
PRIMARY FLIGHT DISPLAY
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
Attitude Indicator with a Ground Pointer Configuration in a Left Turn
Roll Scale Zero Pointer
Roll Scale
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
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Roll Pointer pointing towards the sky.
Roll Scale Zero Pointer
Roll Pointer
Roll Scale
Attitude Indicator with a Sky Pointer Configuration in a Left Turn
The Slip/Skid Indicator is the bar beneath the roll pointer. The indicator moves
with the roll pointer and moves laterally away from the pointer to indicate lateral
acceleration. Slip/skid is indicated by the location of the bar relative to the pointer.
PRIMARY FLIGHT DISPLAY
One bar displacement from the roll pointer is equivalent to one ball displacement
on a traditional Slip/Skid Indicator.
The top of the HSI displays current heading, current GPS track (magenta
diamond), heading trend, and turn rate markings. The heading trend indicates
the rate of turn. Marking for rate of turn are provided at half-standard (1.5°/sec)
and standard (3°/sec) rate.
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G500/600 Cockpit Reference Guide
13
PRIMARY FLIGHT DISPLAY (PFD)
Current HeadingTurn Rate Markings
Heading TrendCurrent GPS Track
HSI Heading Markings
NOTE: If magnetic heading is lost, GPS ground track will be displayed
in place of heading.
Adjusting the Course Pointer
Press the CRS key and turn the PFD knob to select a course for a VOR/ILS or
OBS mode course.
HSI Bearing Pointers
NOTE: The Bearing Pointer for navigation source 1 (BRG1) will be an
arrow with a single line. The Bearing Pointer for navigation source 2
(BRG2) will be an arrow with a double line.
To toggle between the available bearing pointers, press the PFD soft key, then
the BRG soft key, and then the BRG1 or BRG2 soft keys.
PRIMARY FLIGHT DISPLAY
The BRG1 soft key cycles through modes NAV1 and GPS1. Additionally, ADF
is available if an ADF source is installed.
The BRG2 soft key cycles through modes, NAV2 and GPS2 if a second NAV
or GPS source is available. Additionally, ADF is available if an ADF source is
installed.
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
BRG2 Pointer
Bearing Pointers on the HSI
BRG1 Pointer
Selected source for
BRG 2 bearing pointer
Selected
source for
BRG 1 bearing
pointer
PRIMARY FLIGHT DISPLAY
GPS1
GPS2
VOR1
VOR2
LOC1
LOC2
190-00601-03 Rev G
CDI SourceGPS Mode
GPS Advisory
LOI
MSG
LOI
PFD HSI Annunciations
G500/600 Cockpit Reference Guide
Suspend
OCN
ENR
TERM
APR
LNAV
LNAV+V
LNAV/VNAV
LPV
LP
LP +V
1.00nm
0.30nm
OBS
SUSP
15
PRIMARY FLIGHT DISPLAY (PFD)
CDI Source
The CDI Source on the HSI will display which navigation source is selected.
Navigation sources available: GPS1, VOR1, or LOC1.
Navigation sources available: GPS2, VOR2, or LOC2, if a second source is available.
GPS Mode
The GPS Mode annunciation on the HSI indicates the current CDI scaling of the
GPS navigator. See the GPS navigator pilot’s guide for a description of each mode.
GPS Advisory
MSG: Displays when a new advisory message is displayed on the GPS navigator.
LOI (Loss of Integrity): Displays when GPS integrity is lost.
Suspend
OBS: Displays when OBS mode is activated.
SUSP: Displays when automatic waypoint sequencing on the interfaced GPS unit is
suspended.
Marker Beacon Annunciations
PRIMARY FLIGHT DISPLAY
Current
Beacon
Inner Marker
Middle Marker
Outer Marker
16
Marker Beacon
Location
Marker Beacon Location
Marker Beacons
Icon (Standard)Icon (Blink)
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Miscompare Annunciations
For complete description and conditions of miscompare annunciations, see
the G500/600 Pilot’s Guide, P/N 190-00601-02.
Pitch and Roll Miscompare
PRIMARY FLIGHT DISPLAY
Pitch Miscompare
Miscompare Annunciations
Roll Miscompare
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G500/600 Cockpit Reference Guide
17
PRIMARY FLIGHT DISPLAY (PFD)
GPS
NAVIGATOR 2
VLOC
NAVIGATOR 2
GPS
NAVIGATOR 1
VLOC
NAVIGATOR 1
Switching Between Navigation Sources
CDI Sources
The Course Deviation Indicator (CDI) can display two sources of navigation:
GPS or NAV (VOR or LOC). Press the CDI soft key to toggle between the available
CDI modes, (GPS or VOR).
If a second GPS source or NAV source is available, pressing the 1 - 2 soft key
will toggle the navigation sources (VOR1 and VOR2, or GPS1 and GPS2).
PRIMARY FLIGHT DISPLAY
NOTE: Verify the navigation source by the indication on the HSI.
18
NOTE: The selected navigator is the source for all PFD and MFD
functions, except for bearing pointers and external TAWS PFD
annunciations.
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Autopilot (AP)
The G500/600 is able to interface to certain autopilot systems to provide the
functions described in this section. Please refer to your particular Airplane Flight
Manual and autopilot documentation for specific information and operating
instructions.
GAD 43 Attitude
If the GAD 43 Adapter is providing attitude to the autopilot, test the disconnect
mechanism prior to each flight in the following manner:
1) Allow all avionics to complete power up and begin normal operation.
2) Engage the autopilot while on the ground.
PRIMARY FLIGHT DISPLAY
3) Press and release the AP TEST soft key and verify that the autopilot
disconnects normally.
NOTE: If the AP TEST soft key is held for longer than one second, the test
will not run.
CAUTION: Do not use the autopilot if the AP TEST key fails to disconnect
the autopilot.
Autopilot Disconnect
When the GDU 620 attitude monitors have detected an AHRS malfunction,
or the inability to actively monitor the AHRS, a “Check Attitude” annunciation
will be displayed on the PFD and the autopilot will automatically disconnect.
NOTE: Only appears with the installation of an optional GAD 43
Adapter.
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Check Attitude Annunciation
G500/600 Cockpit Reference Guide
19
PRIMARY FLIGHT DISPLAY (PFD)
Heading
The GDU 620 heading bug may be used in conjunction with the “Heading”
mode of supported autopilots. When the autopilot is in “heading” mode and the
heading bug is adjusted in the normal manner, and the autopilot will turn to and
maintain the selected heading. Refer to the Airplane Flight Manual and autopilot
system documentation for instructions on how to use the autopilot heading mode
Selected Heading Box on HSI
.
Altitude Capture (Optional Upgrade)
Adjust the altitude bug in the normal manner when using the altitude capture
interface. Some autopilot installations support arming and disarming of the
selected altitude using the
indicate when this function is available. The selected altitude may be alternately
armed or disarmed by pressing and holding the ALT key on the PFD bezel.
ALT
key on the PFD. The PFD knob window will
PRIMARY FLIGHT DISPLAY
Arm/Disarm Altitude Bug
Autopilot Navigation
The GDU 620 acts as a switching source between the installed navigation
sources (e.g. GPS/VLOC 1-2). The navigation source that is displayed on the HSI
is sent to the autopilot. Refer to the Airplane Flight Manual and autopilot system
documentation for instructions on how to use the autopilot navigation functions.
1) Set your navigation source and HSI to the desired course.
2) Engage your autopilot in navigation mode.
3) Control your autopilot navigation through the navigation source and the HSI.
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G500/600 Cockpit Reference Guide
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PRIMARY FLIGHT DISPLAY (PFD)
GPSS
The GDU 620 will send the GPSS commands from the displayed GPS source to
the autopilot. For example, if GPS 1 is displayed on the HSI, the GPSS
commands from GPS 1 will be sent to the autopilot. Refer to the Airplane
Flight Manual and autopilot system documentation for instructions on how to
use the autopilot’s GPSS function.
NOTE: GPSS commands are not sent to the autopilot when a VLOC
source is displayed on the HSI.
In installations that use GPSS emulation in combination with the “heading”
mode of the autopilot, GPSS mode may be toggled on/off with an external switch
or by pressing and holding the HDG key on the PFD. If the installation uses the
HDG key on the PFD, the PFD knob window will display the GPSS/HDG mode
options.
NOTE: The GDU 620 has the ability to emulate GPSS roll steering for
autopilots that do not support GPSS. The GDU 620 emulates GPSS by
sending headings to the autopilot that guide turn anticipation.
PRIMARY FLIGHT DISPLAY
GPSS OFFGPSS ON
GPSS Mode Control
When GPSS mode is on, the heading bug on the HSI changes to a hollow
outline and a crossed-out heading bug appears in the PFD Knob Mode Indicator,
indicating that the autopilot is not coupled to the heading bug. The bug is still
controllable and may still be used by the pilot for reference. GPSS is annunciated
in the lower left portion of the PFD. The GPSS mode annunciation depends on
the location of the NAV STATUS information, as shown in the following figure.
NAV Status Style 2
21
190-00601-03 Rev G
NAV Status Style 1
GPSS Mode Annunciations
G500/600 Cockpit Reference Guide
PRIMARY FLIGHT DISPLAY (PFD)
Flight Director Display
Flight director commands are presented as a single cue flight director on the
PFD.
SVT OffSVT On
Flight Director Bars Showing Aircraft Pitch
Vertical Speed Control
The GDU 620 vertical speed bug may be used to control vertical speed with
certain autopilots. Refer to the Airplane Flight Manual and autopilot system
documentation for instructions on how to use the vertical speed mode, if available.
Adjust the vertical speed bug in the normal manner when using the vertical
speed mode interface. Some autopilot installations support engaging/disengaging
the vertical speed mode using the VS key on the PFD. The vertical speed mode
may be alternately engaged or disengaged by pressing and holding the VS key
PRIMARY FLIGHT DISPLAY
on the PFD bezel.
22
Engage/Disengage VS Bug
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
Autopilot Mode Annunciations
Some autopilots support mode annunciations located at the top of the PFD.
Refer to the Airplane Flight Manual and autopilot system documentation for
details on the autopilot mode annunciations.
When autopilot annunciations are displayed at the top of the PFD, the Nav
Status information will be located to the left of the HSI (NAV STATUS Style 2).
Active Mode
Armed Mode
Roll ModesPitch Modes
Autopilot Status
Autopilot Annunciations
Active Mode
Armed Mode
PRIMARY FLIGHT DISPLAY
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G500/600 Cockpit Reference Guide
23
PRIMARY FLIGHT DISPLAY (PFD)
Additional Features
Synthetic Vision Technology™
Synthetic Vision Technology (SVT) is offered as a feature to the G500/600.
SVT is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the PFD.
SVT offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
PRIMARY FLIGHT DISPLAY
Airport
Sign
Zero-Pitch
Line
Flight
Path
Marker
Terrain
Threat
SVT Soft Keys
Synthetic Vision Imagery
NOTE: SVT will become disabled if the databases necessary to display
SVT are unavailable (generating a GDU DB ERR or SVT DISABLED alert)
or AHRS or GPS data is unavailable. SVT may be restored once the
fail conditions are removed by following the steps in “Displaying SVT
Terrain.”
Horizon
Heading
Mark
Obstacle
SVT
Terrain
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
PRIMARY FLIGHT DISPLAY (PFD)
The following features are part of the Synthetic Vision Technology. For more
details refer to the G500/600 Pilot’s Guide, Rev. G or later.
• Flight Path Marker• Airport Signs
• Horizon Heading Marks• Runway Display
• Terrain/Obstacle Display and Alerting• Water
• Three-dimensional Traffic
• Zero-Pitch Line
• Wind Vectors• Altitude Minimums Bug
NOTE: SVT may be deactivated under certain conditions, such as loss of
heading. Once the condition is resolved SVT may restart automatically,
otherwise, to reactivate SVT, press the PFD soft key followed by the
SYN VIS soft key, then the SYN TERR soft key.
NOTE: SVT features are not a substitute for standard course and
altitude deviation information using the CDI, VSI, and VDI.
Displaying SVT™ Terrain
1) Press the PFD soft key.
2) Press the SYN VIS soft key.
PRIMARY FLIGHT DISPLAY
3) Press the SYN TERR soft key.
4) Press the BACK soft key to return to the previous page.
Displaying Heading on the Horizon
1) Press the PFD soft key.
2) Press the SYN VIS soft key.
3) If not already enabled, press the SYN TERR soft key.
4) Press the HRZN HDG soft key.
5) Press the BACK soft key to return to the previous page.
Displaying Airport Signs
1) Press the PFD soft key.
2) Press the SYN VIS soft key.
3) If not already enabled, press the SYN TERR soft key.
4) Press the APTSIGNS soft key.
5) Press the BACK soft key to return to the previous page.
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G500/600 Cockpit Reference Guide
25
MULTI-FUNCTION DISPLAY (MFD)
Multi-Function Display (MFD)
7
6
5
4
1
Multi-Function Display (MFD)
NOTE: In some models or installations, the PFD and MFD and their controls
MULTI-FUNCTION DISPLAY
1
2
3
4
5
6
7
26
are switched to the other side.
Soft Keys
Large MFD knob: Use to move between page groups.
Small MFD knob: Use to move within page groups.
Enter: Validates or confirms a menu selection or data entry.
Clear: Erases information, cancels entries, or removes page menus. Pressing and
holding the CLR key displays the first page of the Map Group.
Menu: Displays configuration items for each page of the page groups.
Range Select: Changes the range on the map pages. Up arrow zooms out, down
arrow zooms in. Also aids in scrolling up and down text pages.
G500/600 Cockpit Reference Guide
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3
190-00601-03 Rev G
MULTI-FUNCTION DISPLAY (MFD)
Page Navigation - Moving Between Pages
Page Group
Turn Large MFD knob
Turn Small MFD knob
Page
1) Turn the large MFD knob to move between page groups.
2) Turn the small MFD knob to change pages within the page group.
NOTE: Page Group and Page are shown at the bottom of the MFD.
Changing Settings within a Page
1) Press the MENU key and make the necessary adjustments with the large
MFD knob and small MFD knobs.
2) Press the small MFD knob to activate editing.
3) Turn the large MFD knob to select the desired item.
4) Turn the small MFD knob to change the highlighted value.
5) Press ENT to accept displayed value or press the small MFD knob to cancel
selection or exit the editing mode.
MULTI-FUNCTION DISPLAY
Default Map Page
Press and hold the
190-00601-03 Rev G
CLR
key to return to the first page of the MAP group.
G500/600 Cockpit Reference Guide
27
MULTI-FUNCTION DISPLAY (MFD)
MFD Soft Key Map
The soft keys available depend on the page displayed and the features available.
The soft key “Alerts” is present on the far right position on all MFD pages.
MAP
Navigation Map 1
Declutter
Map
Traffic
Topo
Terrain
Navigation Map 2
Declutter
Map
Traffic
Topo
Terrain
Split Screen
Declutter
Map
Traffic
Topo
Terrain
Traffic*
* Softkeys depend on configuration
WX
Weather Map 1Weather Map 2Weather Map 3
Legend
FCST Time (XM)
WX Alt Dn
WX Alt Up
Legend
FCST Time (XM)
WX Alt Dn
WX Alt Up
Legend
FCST Time (XM)
WX Alt Dn
WX Alt Up
AUX
External
Video
MULTI-FUNCTION DISPLAY
Video 1
Video 2
Setup
System
Setup
Default Unit
RA Test
Dflt Spd
XM Info
Lock
Channel
CH CH +
DIR CH
AUX
XM Radio
Category
CAT CAT +
ALL
(continued)
Terrain
View
Inhibit
Weather Radar
Volume
Mute
Vol Vol +
360
Arc
Mode
Control
Horizon
Vertical
Back
Presets
PS1
PS2
...
PS15
Active Fpl
28
System StatusPosition Reporting
Info
DB ACTV
DB SYNC
LRU
Wpt Info
INFO/MAP
Rwy/Freq
APT DIR
WX/NOTAM
G500/600 Cockpit Reference Guide
Send
FPL
Charts
NOTAM
Detail
Select
Iridium Phone
Dial
Answer
Hang Up
Vol
Keys
1234 5678 90*#
Header
Plan
Profile
Minimums
ALERTS
TRND/ACK
CAPTURE
BACK
190-00601-03 Rev G
MAP GROUP
Map Group
Navigation Map 1 and Navigation Map 2 Pages
Soft Keys Found on Navigation Map Pages
Moving the Map Pointer Around the Map (Panning)
NOTE: Panning can be used in Terrain pages to view elevation levels.
1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page
Group, press the small MFD knob. A flashing arrow (map pointer) will appear
in the center of the map page.
MAP GROUP: NAV PAGES
2) Turn the large MFD knob to move the map pointer left and
right (horizontally).
Map Pointer
3) Turn the small MFD knob to move the map pointer up and
down (vertically).
4) Press the small MFD knob again to exit panning mode.
Selecting Items on the Map
1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page
Group, while the map pointer is active, move the map pointer to highlight a
waypoint.
2) Press ENT to display information about the highlighted waypoint.
3) Press the INFO soft key (if available) to view more information about the
highlighted waypoint.
4) Press the WX soft key (if available) to view TAF and METAR information. Press
the small MFD knob again to return to the map.
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G500/600 Cockpit Reference Guide
29
MAP GROUP
Decluttering (DCLTR) the Map Pages
There are four levels of decluttering, DCLTR, DCLTR-1, DCLTR-2, and
DCLTR-3. DCLTR shows the most detail while DCLTR-3 removes most detail.
While viewing Navigation Map 1 or Navigation Map 2 page of the Map Page
Group, press the
will toggle through the declutter levels.
Turning on Map Overlays
While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group,
press the
MAP
the appropriate soft key.
Measuring Distances
1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page
Group, press MENU.
2) Turn the large MFD knob or the small MFD knob to highlight “Measure
Bearing/Distance” and then press ENT.
DCLTR
soft key. Each successive press of the
DCLTR
soft key
soft key. Select the Traffic, TOPO, or Terrain overlays by pressing
3) Turn the large or small MFD knobs to move the map pointer. The distance,
bearing, and coordinates are displayed at the top of the screen.
MAP GROUP: SETUP OPTIONS
Distance, Bearing and Coordinates DisplayMeasuring Map Pointer
4) Press ENT to reset the distance and bearing values.
5) Press the small MFD knob to stop measuring.
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
MAP GROUP
Customizing Maps
1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page
Group, press the MENU key.
Map Setup Option Menu
2) Press the ENT key to enter the setup page. The selected group will be
flashing.
3) Turn the small MFD knob to activate the drop down menu and to move
within available groups (Map, Weather, Traffic, or Aviation).
MAP GROUP: SETUP OPTIONS
Available Groups
4) Press the ENT key to select the group and set your preferences.
5) Turn the large MFD knob to move between fields.
6) Turn the small MFD knob to display available options. Press the ENT key to
select your preference and move to the next option.
7) When completed with setting preferences, press the small MFD knob to
return to the Navigation Map 1 page.
8) Repeat the above steps to set preferences for the remaining groups.
NOTE: In the Map Options Setup section, the selected range is defined
as the map range below which the display feature will be visible.
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G500/600 Cockpit Reference Guide
31
MAP GROUP
Map Setup Options
GroupSelections
• Orientation (North Up, Track Up, DTK up, HDG up)
• North Up At (Off to 500 NM)
• Auto Zoom (On or Off)
• Land Data (On or Off)
• Track Vector Length (Off to 20 mins)
• Wind Vector (On or Off)
MAP
• Enhanced Range Ring (On or Off)
• Topo Data (On or Off)
• Topo Scale (On or Off)
• TERRAIN Data (On or Off)
• Obstacle Viewing Range (Off to 15 NM)
• Power Line Viewing Range (Off to 15 NM)
• Lat/Lon Viewing Range (Off to 500 NM)
• Selected Alt Range Arc (On or Off)
• NEXRAD Data Viewing Range (Off to 500 NM)
• NEXRAD Cell Movement (On or Off)
WEATHER
• NEXRAD Legend (On or Off)
• NEXRAD Source (US or Canada)
• XM Lightning Viewing Range (Off to 500 NM)
MAP GROUP: SETUP OPTIONS
TRAFFIC
• Traffic Mode (Off, All Traffic, TA/PA, TA Only)
• SafeTaxi Viewing Range (Range: Off to 2.5 NM)
• RWY Extension Range (Range: Off to 2.5 NM)
• INT/NDB Viewing Range (Range: Off to 15 NM)
• VOR Viewing Range (Range: Off to 150 NM)
• Class B/TMA (Range: Off to 500 NM)
• Class C/TCA (Range: Off to 150 NM)
• Class D (Range: Off to 150 NM)
AVIATION
• Restricted (Range: Off to 150 NM)
• MOA (Military) (Range: Off to 150 NM)
• Other/Adiz (Range: Off to 150 NM)
• TFR (Range: Off to 500 NM)
• Airways (Off, All, LO Only, HI Only)
• Smart Airspace (On or Off)
• Show Airspaces (All, Below 18000ft - Below 3000ft)
• Airspace Labels (On or Off)
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G500/600 Cockpit Reference Guide
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MAP GROUP
SafeTaxi® (Optional)
SafeTaxi is an enhanced feature that gives greater map detail when zooming
in on airports at close range. The airport display on the map reveals runways
with numbers, taxiways with identifying letters/numbers, and airport landmarks
including ramps, buildings, control towers, and other prominent features.
Resolution is greater at lower map ranges. When the aircraft location is within the
screen boundary, including within SafeTaxi ranges, an airplane symbol is shown
on the navigation map views for enhanced positional awareness. This database
MAP GROUP: SETUP OPTIONS
is updated on a 56-day cycle.
NOTE: Do not use SafeTaxi or ChartView functions as a basis for
ground maneuvering. SafeTaxi and ChartView functions have not
been qualified to be used as an Airport Moving Map Display (AMMD).
SafeTaxi and ChartView are intended to improve pilot situational
awareness during ground operations and should only be used by the
flight crew to orient themselves on the airport surface.
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G500/600 Cockpit Reference Guide
33
MAP GROUP
Split Screen Page (Optional)
Soft Keys Found on Split Screen Page
External Video is an optional function that displays video provided by an
externally mounted video source on the aircraft.
1) While viewing the Map function, turn the small MFD knob to the third page
of the map group.
Current Video Source
Display of External Video Source
Map Display
MAP GROUP: SPLIT SCREEN PAGE
External Video
2) The External Video page will show the external video on the top half of the
MFD and a Navigation Map will be shown on the lower half.
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
Traffic Map Page (Optional)
Soft Keys Found on Traffic Map Page
MAP GROUP
OPERATESTANDBYMOTION
STANDBY
ABSOLUTE
RELATIVEOFF
ALT MODE
DESELECT
DURATION
BACKBELOWNORMALABOVEUNRSTD
OPR/STBY
Traffic Display
When a traffic alert is generated by an interfaced traffic system, the PFD will
display a traffic annunciator and the MFD will have a pop-up screen displaying
the detected traffic, if not viewing the Traffic page. To remove the pop-up, press
the CLR
window will be removed when the traffic alert is no longer active.
key
. Press the ENT key to go to the traffic page. The traffic pop-up
Traffic Annunciation
Traffic
MAP GROUP: TRAFFIC PAGE
PFD Traffic DisplayMFD Traffic Pop-Up Window
190-00601-03 Rev G
Traffic Pop-Up
G500/600 Cockpit Reference Guide
35
MAP GROUP
Displaying and Operating Traffic Advisory Systems (TAS)
Operating
Mode
Range Ring
Non-Threat
Traffic
Ownship
Symbol
Proximity
Advisory,
Aircraft is 5000
ft Above and
Descending
Non-Bearing Traffic (System is Unable to Determine Bearing),
Aircraft Distance is 8.0 NM, 1100 ft Above and Descending
Traffic Map - TAS
Traffic Advisory,
Off Scale Aircraft
is Out of Range,
1200 ft Above and
Climbing
Traffic Advisory,
1200 ft Above and
Climbing
Traffic Mode Field
MAP GROUP: TRAFFIC PAGE
36
NOTE: Depending on your traffic configuration, the OPERATE and
STANDBY soft keys may not be available.
Altitude Mode Field
NOTE: Some traffic systems will not enter standby mode while
airborne.
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
MAP GROUP
Press the ALT MODE soft key to change what traffic is displayed. Pressing the
BELOW, NORMAL, ABOVE or UNRSTD soft keys will determine what traffic
is displayed. The selection is shown in the altitude mode field. The values below
define what each altitude mode displays, relative to the altitude of the aircraft.
Soft KeyDescription
BELOWDisplays traffic from -9900 to +2700 ft
NORMALDisplays traffic from -2700 to +2700 ft
ABOVEDisplays traffic from -2700 to +9900 ft
UNRSTDAll traffic is displayed (unrestricted) from +/-9900 ft
TAS Test Mode (On Ground)
MAP GROUP: TRAFFIC PAGE
1) While viewing the Traffic Map Page of the Map Page Group, press the MENU
key and select Test Mode from the menu.
2) Verify that a traffic message is shown next to the altitude tape on the PFD
and that the traffic pop-up is displayed on the MFD.
After a few seconds, test mode is exited automatically by the traffic system.
Traffic Annunciation
Traffic Annunciation on PFD
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G500/600 Cockpit Reference Guide
37
MAP GROUP
TIS Traffic
The Traffic Map Page is configured to show surrounding TIS traffic data in
relation to the aircraft’s current position and altitude, without clutter from the
basemap. Aircraft orientation on this map is always heading up unless there is
no valid heading.
TIS receives traffic information from ground stations, and is updated every five
seconds. The GDU 620 displays up to eight traffic targets within a 7.5-NM radius,
from 3000 feet below to 3500 feet above the requesting aircraft.
Displaying TIS Traffic
While viewing the Traffic Page of the Map Page Group
press the OPERATE
soft key to begin displaying traffic. “TIS OPER” is displayed in the upper left
hand corner of the MFD.
NOTE: TIS is disabled when a Traffic Advisory System (TAS) is installed.
Operating
Mode
MAP GROUP: TRAFFIC PAGE
38
G500/600 Cockpit Reference Guide
Traffic Advisory,
Aircraft is 1200 feet
above, climbing,
and moving in the
direction of the line
Proximity Advisory,
Aircraft is 3000 feet
above, descending,
and moving in the
direction of the line
190-00601-03 Rev G
MAP GROUP
ADS-B Traffic (Optional)
The ADS-B traffic page provides an enhanced display of traffic from a
compatible ADS-B In system. Available ADS-B traffic features may include
individual target selection and other details, such as type, direction, groundspeed,
and motion.
ADS-B and TCAS
Status and Altitude
Filter
Map
Orientation
Range Ring Radius
Selected
Traffic Info
MAP GROUP: TRAFFIC PAGE
Basic Directional
Traffic, 4000 ft
Below and
Climbing
Selected Vector
Motion and
Duration
NOTE: ADS-B targets will be shown as the filled-in icon when they are
within 6NM laterally and 1200 ft vertically of the ownship; otherwise,
they are shown as the hollow icons.
Traffic Motion
Vector
Ownship
Icon
Range Rings
Turn Cursor
Knob for Next
Target
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G500/600 Cockpit Reference Guide
39
MAP GROUP
ADS-B Target Selection
Traffic targets displayed on the dedicated traffic page may be selected in order
to obtain additional information about a traffic target.
1) Press the small MFD knob to start target selection.
2) Turn the small or large MFD knobs to step through selection of the available
targets.
3) Press the small MFD knob to stop target selection. Press the DESELECT key to
stop selection and/or clear target selection.
ADS-B Status
ADS-B Status displays the current status of traffic application: Off, Surface,
Airborne, Fail, Test, or N/A.
TAS/TCAS/TCAD Status
This shows the current operating mode/status of an interfaced TAS/TCAS/
TCAD system: STBY, GND, APR, OPER, or FAIL.
ADS-B Motion Vector
When Absolute Motion Vectors are selected, the vectors extending from the
traffic targets depict the target reported track and speed over the ground. When
Relative Motion Vectors are selected, the vectors extending from the traffic targets
display how the traffic target is moving relative to your aircraft. These vectors are
calculated using the traffic target’s track and ground speed and your aircraft’s track
and ground speed. These two values are combined to depict where the traffic target
MAP GROUP: TRAFFIC PAGE
is moving purely with respect to your aircraft and give a forecast of where the traffic
target will be, relative to your aircraft, in the near future.
40
NOTE: Absolute motion vectors are the same color as the traffic target.
Relative motion vectors are yellow for TAs and otherwise are green. The
annunciation on the bottom of the dedicated traffic page indicates which
vector type is selected and their length.
NOTE: Relative motion vectors are not available on the ground.
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
MAP GROUP
Terrain/TAWS-B Page
(Optional)
Soft Keys Found on Terrain/TAWS-B Page
VIEW360
Garmin provides the following Terrain/TAWS selections, based upon your
system configuration.
ARCINHIBIT
MAP GROUP: TERRAIN/TAWS-B PAGE
WARNING: Do not use Terrain-SVT information for primary terrain
avoidance. Terrain-SVT is intended only to enhance situational
awareness.
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.
NOTE: TAWS alerts will be generated by the GPS TAWS unit on
the PFD if an external TAWS unit is installed and interfaced to the
G500/600.
• TERRAIN-PROXIMITY - is a non-TSO-C151b certified terrain awareness
system. Do not confuse Terrain Proximity with TAWS. TAWS is TSOC151b certified and Terrain Proximity is not. Terrain Proximity does
not provide warning annunciations or voice alerts, it only provides
color indications on map displays when terrain and obstacles are within
a certain altitude threshold from the aircraft.
• TERRAIN-SVT - refers to a subset of Class B TAWS that meets the terrain
alerting requirements outlined in Section 7.b of AC 23-26. Terrain-SVT
is a non-TSO-C151b certified terrain awareness system. Do not confuse
Terrain-SVT with TAWS. TAWS is TSO-C151b certified and TerrainSVT is not. Terrain-SVT is a subset of Class B TAWS that provides a
190-00601-03 Rev G
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41
MAP GROUP
Class B TAWS FLTA functionality, including visual alerting and aural
alerting. Terrain-SVT is provided with the Synthetic Vision functionality
and not marketed separately. Garmin Terrain-SVT is available in GDU
620 v3.00 or later, with SVT enabled.
• TAWS-B - is an optional feature developed that meets the terrain alerting
and ground proximity requirements for Class B TAWS system as defined
in TSO-C151b.
Viewing Terrain
NOTE: Obstacles/Wires will be removed from the Terrain/TAWS page
when range
(
RNG
)
exceeds 10 NM.
While viewing the Terrain/TAWS-B page of the Map Page Group, press the
VIEW soft key and then press the 360 or ARC soft keys to select the desired view.
360 or ARC Soft Keys
Pressing the INHIBIT soft key, deactivates the PDA/FLTA aural and visual alerts.
See AFMS for guidance on inhibiting TAWS.
Inhibit Soft Key
Press
MENU
for selections to hide or show Aviation Data Overlay on the
Terrain page.
NOTE: Installations with a valid external TAWS-B source will not
display the INHIBIT key.
MAP GROUP: TERRAIN/TAWS-B PAGE
Aviation Data Overlay
42
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
Terrain Pop-Up Alerts
MAP GROUP
MAP GROUP: TERRAIN/TAWS-B PAGE
TERRAIN-SVT Pop-Up Alert on MFD
TAWS-B Pop-Up Alert on MFD
TERRAIN-SVT™ Pop-Up Alert
TERRAIN-SVT alerts typically employ a CAUTION or a WARNING alert severity
level, or both. When an alert is issued, visual annunciations are displayed and
aural alerts are simultaneously issued. Refer to the Alerts section of this guide
for more information on alerts, both visual and aural. When an alert is issued,
annunciations appear on the PFD and MFD (TAWS page only). If the TERRAINSVT Page is not displayed at the time, a pop-up alert appears on the MFD. To
acknowledge the pop-up alert and return to the currently viewed page, press the
CLR key. To acknowledge the pop-up alert and go to the TERRAIN-SVT page,
press the ENT key.
TAWS-B Pop-Up Alert
TAWS-B alerts typically employ a CAUTION or a WARNING alert severity
level, or both. When an alert is issued, visual annunciations are displayed and
aural alerts are simultaneously issued. Refer to the Alerts section of this guide
for more information on alerts, both visual and aural. When an alert is issued,
annunciations appear on the PFD and MFD (TAWS page only). If the TAWS-B Page
is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge
the pop-up alert and return to the currently viewed page, press the CLR key. To
acknowledge the pop-up alert and go to the TAWS-B page, press the ENT key.
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43
WX GROUP
WX Alt Up
WX Group
XM Weather Map Pages
Soft Keys Found on XM Weather Map Pages
LEGEND
NOTE: The preferences set on XM Weather Map pages are unique to
each page.
FCST TIME
WX Alt Dn
Customizing the Weather Map
1) While viewing any of the XM Weather Map pages in the WX Page Group,
press the MENU key to display the page menu. Press ENT.
2) Turn the small MFD knob to select Weather Setup 1 or Weather Setup 2 and
press ENT.
WX GROUP: XM WEATHER PAGES
3) Turn the large MFD knob to select desired item to change. Turn the small
MFD knob to set the preference of the weather feature option.
4) Press ENT to confirm your selection.
5) To return to the XM Weather Map page, press the small MFD knob.
44
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
XM Weather Items
WX Page Menu - Weather Setup
Menu ItemAdjustment
Map OrientationNorth Up, Track Up
NEXRAD Data Viewing RangeOff, 10 NM to 500 NM
NEXRAD LegendOn/Off
SourceUS, Canada
Echo Top Data Viewing RangeOff, 10 NM to 500 NM
Cloud Top Data Viewing RangeOff, 10 NM to 500 NM
Lightning Data Viewing RangeOff, 10 NM to 500 NM
Cell Mov Data Viewing RangeOff, 10 NM to 500 NM
SIG/AIR Viewing RangeOff, 10 NM to 500 NM
PIREPS Data Viewing RangeOff, 10 NM to 500 NM
METAR Data Viewing RangeOff, 10 NM to 500 NM
Surface Data Viewing RangeOff, 10 NM to 500 NM
Frz Lvl Data Viewing RangeOff, 10 NM to 500 NM
Wnds Aloft Data Viewing RangeOff, 10 NM to 500 NM
County Data Viewing RangeOff, 10 NM to 500 NM
TFR Data Viewing RangeOff, 10 NM to 500 NM
AIREPS Data Viewing rnageOff, 10 NM to 500 NM
Icing Data Viewing RangeOff, 10 NM to 500 NM
Turbulence Data Viewing RangeOff, 10 NM to 500 NM
Cyclone Data Viewing RangeOff, 50 NM to 500 NM
WX GROUP
WX GROUP: XM WEATHER PAGES
NOTE: Due to similarities in color schemes, it is not possible to display
NEXRAD Data and Echo Top Data at the same time.
NOTE: Due to similarities in color schemes, it is not possible to display
Echo Top Data and Cloud Top Data at the same time.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
45
WX GROUP
Weather Legend
A mini-legend can be displayed on the XM Weather Map
page upper right hand corner for the weather products you
selected in the setup menu.
To view a full page legend:
1) While viewing any of XM Weather Map pages in the WX
Page Group, press the LEGEND soft key.
2) Turn the small MFD knob or large MFD knob to view
the entire legend.
3) Exit and return to the map page by pressing either the
LEGEND soft key, ENT key, or the small MFD knob.
Mini-Legend
Changing Forecast Time
1) When the Surface Data products (Surface Analysis and City Forecasts) are
displayed, the time period for these forecasts can be changed with the FCST TIME soft key.
2) Press the FCST TIME soft key to cycle through the age of the information in
WX GROUP: XM WEATHER PAGES
12 hour increments from CURRENT to 48 HR.
Changing Weather Altitude
1) When Winds Aloft, Turbulence, or Icing products are displayed, the altitude for
these forecasts can be selected with the WX Alt Up/Dn soft keys.
2) Press the WX Alt Dn or WX Alt Up soft keys to cycle through the available
forecast periods as shown on the right side of the weather page.
46
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
WX GROUP
Garmin Flight Data Services (GFDS) Map Pages
Soft Key Found on GFDS Weather Map Pages
WX GROUP: GFDS PAGES
Requesting Garmin Flight Data Services (GFDS)
Prior to requesting GFDS information, an access code and system ID will need
to be assigned. For more information on GFDS and how to register, see the latest
revision of the G500/600 Pilot’s Guide, P/N 190-00601-02.
After registering you are able to display GFDS data:
1) While viewing any one of the three pages of the WX Group, press the MENU
button.
2) Highlight GFDS Data Request and press the ENT button to display the GFDS
DATA REQUEST page.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
47
WX GROUP
Coverage
Area
Coverage Area
Distances:
Remaining FPL,
Next 50 NM -
Next 500 NM
Width of Coverage:
50 NM - 500 NM
Update Rate:
Off - 60 Minutes
Manual
Request
GFDS Data Request Page
Cancel Manual
Request
Status of Request
Configuring GFDS Data Request Page
1) Turn the large MFD knob to the Coverage box. Press ENT to select or
deselect the coverage areas. Selected coverage areas are denoted by a green
WX GROUP: GFDS PAGES
check mark.
2) Turn the large MFD knob to the Auto Request box and press ENT to change
the update rate to either OFF or ON.
3) Turn the large MFD knob to the Manual Request box and press ENT to either
send request or cancel current request.
4) Press the small MFD knob to return to the GFDS page.
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G500/600 Cockpit Reference Guide
190-00601-03 Rev G
FIS-B Weather Map Pages
Soft Keys Found on FIS-B Weather Map Pages
WX GROUP
WX GROUP: FIS-B WEATHER PAGES
LEGEND
NOTE: The preferences set on FIS-B Weather Map pages are unique to
each page.
FCST TIME
WX Alt DnWX Alt Up
Customizing the Weather Map
1) While viewing any of the FIS-B Weather Map pages in the FIS-B Page Group,
press the MENU key to display the page menu.
2) Turn the small MFD knob to select Weather Setup and press ENT.
3) Turn the large MFD knob to select the desired item to change. Turn the small
MFD knob to set the preference of the weather feature option.
4) Press ENT to confirm your selection.
5) To return to the FIS-B Weather Map page, press the small MFD knob.
190-00601-03 Rev G
G500/600 Cockpit Reference Guide
49
WX GROUP
FIS-B Weather Items
WX Page Menu - Weather Setup
Menu ItemAdjustment
Map OrientationNorth Up, Track Up
NEXRAD Data Viewing RangeOff, 10 NM to 500 NM
NEXRAD LegendOn/Off
SourceCONUS, Regional, Combined
SIG/AIR Viewing RangeOff, 10 NM to 500 NM
PIREPS Data Viewing RangeOff, 10 NM to 500 NM
METAR Data Viewing RangeOff, 10 NM to 500 NM
Wnds Aloft Data Viewing RangeOff, 10 NM to 500 NM
TFR Data Viewing RangeOff, 10 NM to 500 NM
WX GROUP: FIS-B WEATHER PAGES
50
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
Weather Radar (Optional)
Weather Radar Map Page
Soft Keys Found on Weather Radar Map Page
WX GROUP
WX GROUP: WEATHER RADAR
Operating
Mode
Weather
Alert
(GWX only)
Precipitation
Scale
Operating
Mode
Control
Window
190-00601-03 Rev F
Weather Radar
G600 Cockpit Reference Guide
51
WX GROUP
Airborne Color Weather Radar
WARNING: Begin transmitting only when it is safe to do so. If transmitting
on the ground is necessary, ensure that no personnel or objects are within
the minimum safe distance from the radar antenna. For Garmin GWX radars,
the minimum safe distance may be up to 14 feet. For 3rd-party radars,
refer to the radar pilot’s guide or other manufacturer documentation to
determine the minimum safe dis-tance.
CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always recommended to put the radar in Standby Mode before taxiing
the aircraft to prevent the antenna from bouncing on the bottom stop and
possibly causing damage to the radar assembly.
Displaying Weather on the Weather Radar Page
1) Turn the large MFD knob to select the last page of the WX Page Group.
2) Press the MODE soft key.
3) If the aircraft is on the ground, press the STANDBY soft key to initiate the
warm-up period. After the warm-up is complete, the radar enters Standby
Mode. After the aircraft is airborne, press the WEATHER soft key.
OR
WX GROUP: WEATHER RADAR
If the aircraft is already airborne, press the
WEATHER or GROUND soft key.
The warm-up period is initiated, after which the radar begins transmitting.
The horizontal scan is initially displayed. Press the BACK soft key, then the
VERTICAL soft key to scan vertically.
4) Press the RNG keys to select the desired range.
Adjusting Antenna Tilt
1) Press and turn the small MFD knob to adjust the tilt of the antenna up or
down. Monitor the displayed tilt value in the TILT field. The range of tilting the
antenna is DN 15° to UP 15°.
2) Press the small MFD knob to confirm selection.
52
G600 Cockpit Reference Guide
190-00601-03 Rev F
WX GROUP
Adjusting the Antenna Bearing
1) Press the small MFD knob and turn the large MFD knob to move to the
BEARING field.
2) Adjust the azimuth position of the antenna right or left. Monitor the displayed
bearing value in the BEARING field. The range of the bearing is R45° to L45°.
3) Press the ENT key to remove the cursor.
When scanning horizontally, a bearing line may be displayed to aid in
positioning the antenna for the vertical scan. If the Bearing Line is not displayed,
WX GROUP: WEATHER RADAR
perform the following steps:
1) Press the CONTROL soft key.
2) Press the BRG soft key.
Sector Scan (GWX Radars Only)
1) Press the small MFD knob and turn the large MFD knob to move to the
SECTOR SCAN field.
2) Turn the small MFD knob to select FULL, 60°, 40°, or 20° scan.
3) If desired, readjust the Bearing Line to change the center of the Sector Scan.
Turn the large MFD knob to move cursor to the BEARING field and turn the
small MFD knob to adjust the line.
Adjusting Gain
WARNING: Changing the gain in Weather Mode (Garmin GWX units only)
causes precipitation intensity to be displayed as a color not representative
of the true intensity. Remember to return the gain setting to “Calibrated”
for viewing the actual intensity of precipitation.
1) Press the small MFD knob and turn the large MFD knob to move to the
GAIN field.
2) Turn the small MFD knob to adjust the gain for the desirable level. The gain
setting is visible in the gain field as a movable horizontal bar in a flashing
box. The line pointer is a reference depicting the calibrated position.
3) Press the ENT key to remove the cursor.
4) To restore the gain to the calibrated position, press the GAIN CAL soft key.
190-00601-03 Rev F
G600 Cockpit Reference Guide
53
WX GROUP
Antenna Stabilization
1) To activate or deactivate the antenna stabilization, press the CONTROL soft
key.
2) Press the STAB ON soft key to activate antenna stabilization or press the STAB OFF soft key to deactivate. The current stabilization condition is shown
in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH™) (GWX Weather
Radar only)
WATCH (Weather Attenuated Color Highlight) which helps identify possible
“shadowing” effects of short-range cell activity – identifying areas where radar
return signals are weakened, or attenuated, by intense precipitation (or large areas
of lesser precipitation) and may not fully reflect the “storm behind the storm”.
To activate the WATCH feature, press the CONTROL soft key. Press the WATCH
soft key. Press the WATCH soft key again to deactivate.
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system automatically switches to Standby Mode.
Altitude Compensated Tilt (ACT) - GWX 70 only
Altitude Compensated Tilt (ACT) automatically adjusts the tilt to compensate
for altitude changes as you climb or descend.
Turbulence Detection - GWX 70 only (optional)
WX GROUP: WEATHER RADAR
Turbulence Detection activates a feature that detects and displays severe
turbulence. Turbulence Detection is inactive at ranges greater that 160 NM. This
optional feature requires a separate enablement. See your dealer for details. If
Turbulence Detection is enabled and available, Turbulence Detection will be
reported as Inactive in any of the following conditions:
• Scan orientation is not Horizontal
• Scan range is greater than 160 NM
• Radar mode is not Weather
Ground Clutter Suppression (GCS) - GWX 70 only (optional)
Ground Clutter Suppression reduces the amount of returns as a result of highly
reflective objects on the ground, such as buildings or cities, while maintaining
the intensity and size of weather returns. his optional feature requires a separate
enablement. See your dealer for details.
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G600 Cockpit Reference Guide
190-00601-03 Rev F
AUX GROUP
Aux Group
External Video Page (Optional)
Soft Key Found on External Video Page
Setting Brightness, Contrast, and Saturation Levels
The following steps can be applied to either Video 1 or Video 2.
1) While viewing the External Video Page of the Aux Page Group, press the
desired video soft key (VIDEO 1, VIDEO 2, or FULL).
2) Press the SETUP soft key. The BRIGHTNESS in the CURRENT box will flash.
Turn the small MFD knob to change the brightness of the video output.
3) Turn the large MFD knob to CONTRAST and turn the small MFD knob to
change the contrast level of the video output.
AUX GROUP: SYSTEM SETUP PAGE
4) Turn the large MFD knob to SATURATION and turn the small MFD knob to
change the saturation level of the video output.
5) Press the small MFD knob to exit out of the setup mode.
Setting the Zoom Level of the Video Output
1) While viewing the External Video Page of the Aux Page Group, press the small
MFD knob.
2) Press the RNG (Range) keys to zoom in and out. The range of the zoom
feature is 1x up to 10x.
3) Press the small MFD knob to exit.
Setup Soft Key
Video Soft Keys
190-00601-03 Rev G
Full Soft Key
G500/600 Cockpit Reference Guide
55
AUX GROUP
System Setup Page
Soft Keys Found on System Setup Page
Setting Brightness and Mode
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob. The LEVEL in the DISPLAY BRIGHTNESS box will flash.
2) Turn the small MFD knob to brighten or dim the display.
3) Press ENT when you reach the desired level.
NOTE: When LEVEL is changed, the MODE defaults to MANUAL. If
MODE is set the AUTO, the LEVEL will adjust in response to ambient
light or a lighting bus, as configured during installation.
Setting Airspeed References
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob. Turn the large MFD knob to move to the desired field in the
AIRSPEEDS box.
2) Turn the small MFD knob to change the speeds and to also turn the speeds
ON or OFF. When the speeds are turned ON they are shown near the bottom
of the Airspeed Tape if airspeed is zero.
AUX GROUP: SYSTEM SETUP PAGE
Airspeed ReferencesV Speed References on Airspeed Tape
NOTE: At any time during the setting of your airspeed references,
pressing the
configuration.
56
DFLT SPD
G500/600 Cockpit Reference Guide
soft key will restore the unit to its initial
190-00601-03 Rev G
AUX GROUP
Selecting Wind Vector Styles
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob and turn the large MFD knob to move to the field in the PFD
OPTIONS box.
2) Turn the small MFD knob to select the styles available for displaying wind
vectors. Each style shows direction and velocity of the wind.
Style 1Style 2Style 3Style 4
AUX GROUP: SYSTEM SETUP PAGE
Style 1
Style 2
Style 3
Style 4
Displays headwind and crosswind components
Displays total wind direction and speed.
Displays total wind direction with headwind and crosswind speed components.
Displays total wind direction in degrees with wind speed.
Selecting NAV Status Styles
When selected, Nav Status information is displayed on the PFD either on the
top of the display (Style 1) or to the left of the HSI (Style 2).
1) While viewing the System Setup page of the AUX page group, press the small
MFD knob to activate the cursor.
2) Turn the large MFD knob to highlight the desired NAV Status value.
3) Turn the small MFD knob to select the style and press ENT
.
190-00601-03 Rev G
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57
AUX GROUP
Selecting Temperature Reference
1) While viewing the System Setup page of the AUX page group, press the small
MFD knob to activate the cursor. Turn the large MFD knob to highlight the
desired Temp Reference value.
2) Turn the small MFD knob to select the Temp Reference type and press ENT
Figure 3-44 Outside Air Temperature Selection
Synchronization (For Dual Installations Only)
NOTE: The SYNCHRONIZATION option will only be available if a
second GDU 620 is installed.
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob and turn the large MFD knob to move to the desired field in the
SYNCHRONIZATION box.
2) Turn the small MFD knob to turn ON or OFF synchronization of the CDI. Turn
the large MFD knob to move to the BARO setting. Turn the small MFD knob
to turn the synchronization of the barometer ON or OFF. Turn the small MFD
knob to turn the synchronization of databases ON or OFF.
3) Press ENT to move to the DATE/TIME box or press the small MFD knob to
AUX GROUP: SYSTEM SETUP PAGE
exit the editing mode.
.
58
Synchronization Option
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
AUX GROUP
Setting Time Format
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob. Turn the large MFD knob to the desired field in the DATE/TIME
box. The only items that are able to be modified is the TIME FORMAT and
TIME OFFSET. The date and time are coordinated with the GPS.
2) Turn the small MFD knob to display your choices of LOCAL 12hr, LOCAL
24hr, and UTC (Universal Time, Coordinated). Turn the small MFD knob to the
desired format and press ENT to confirm your selection.
Setting Time Offset
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob. Turn the large MFD knob to the time offset portion of the DATE/
TIME box.
2) Use the small MFD knob and large MFD knob to edit the time offset.
3) Press ENT to confirm your selection. Press the small MFD knob to exit the
editing mode.
To convert UTC to local time, a time offset must be chosen. See the table below
to determine the time offset.
Time ZoneStandard Local Time OffsetDaylight Saving Time Offset
Atlantic -4 hours-3 hours
Eastern-5 hours-4 hours
Central-6 hours-5 hours
Mountain-7 hours-6 hours
Pacific-8 hours-7 hours
Alaskan-9 hours-8 hours
Hawaiian-10 hours-9 hours
AUX GROUP: SYSTEM SETUP PAGE
190-00601-03 Rev G
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59
AUX GROUP
MFD Display Units
NOTE: At any time during the setting of your preferences, pressing
the
DFLT UNIT
synchronization, time format, time offset and display units to the initial
settings.
NOTE: The corresponding GPS navigator must also be set to match
the selection chosen (distance, speed, NAV angle, pressure, and
temperature units) on the GDU 620.
Setting Distance and Speed Units
soft key will restore the settings for brightness,
1) Press the small MFD knob and turn the large MFD knob to move to the MFD
DISPLAY UNITS box.
2) Turn the small MFD knob to display your choices of IMPERIAL, METRIC, and
NAUTICAL units for distance and speed displayed on MFD. Press ENT to
confirm your selection. Press the small MFD knob to exit editing mode.
Setting Altitude and Vertical Speed Units
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob and turn the large MFD knob to move to the desired field of the
MFD DISPLAY UNITS box.
2) Turn the small MFD knob to display your choices of FEET or METRIC units
for altitude and vertical speed. Press ENT to confirm your selection. Press the
small MFD knob to exit editing mode.
Setting Nav Angle
1) While viewing the System Setup Page of the Aux Page Group, press the small
AUX GROUP: SYSTEM SETUP PAGE
MFD knob and turn the large MFD knob to move to the desired field of the
SYSTEM DISPLAY UNITS box.
2) Turn the small MFD knob to display your choices of MAGNETIC(°) or TRUE (°)
measurement for navigating. Press ENT to confirm your selection and move
to the next preference or press the small MFD knob to exit editing mode.
Setting Pressure Units
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob and turn the large MFD knob to move to the desired field of the
SYSTEM DISPLAY UNITS box.
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G500/600 Cockpit Reference Guide
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AUX GROUP
2) Turn the small MFD knob to display your choices of INCHES(in) or
HECTOPASCALS (hpa) for your barometric pressure units. Press ENT to confirm
your selection and move to the next preference or press the small MFD knob
to exit editing mode.
Setting Temperature Units
1) While viewing the System Setup Page of the Aux Page Group, press the small
MFD knob and turn the large MFD knob to move to the desired field of the
SYSTEM DISPLAY UNITS box.
2) Turn the small MFD knob to display your choices of CELSIUS(°C) or
FAHRENHEIT(°F) for the temperature. Press ENT to confirm your selection and
AUX GROUP: SYSTEM SETUP PAGE
press the small MFD knob to exit editing mode.
Data Link
1) Press the small MFD knob and turn the large MFD knob to move to the Data
Link box.
2) Turn the small MFD knob to display your choices of the available WX/TFR
Source. Press ENT to confirm your selection. Press the small MFD knob to exit
editing mode.
Radar Altimeter Test
NOTE: Not all radar altimeters have the test function.
Press the RA TEST soft key (if available) to activate the radar altimeter test.
An RA TEST annunciation will be displayed on the PFD. For more information
on the Radar Altimeter and its settings, see the latest revision of the G500/600
Pilot’s Guide, P/N 190-00601-02.
RA TEST Annunciation on PFD
If the unit fails the self-test, the RA FAIL annunciation will appear on the
PFD.
RA FAIL Annunciation on PFD
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AUX GROUP
XM® Information Page (Optional)
Soft Key Found on XM Information Page
While viewing the Aux Group, turn the small
MFD knob
to display the XM
Information screen. This page contains the Data Radio and Audio Radio IDs. The
only option on this page is to
LOCK
in your information once your subscription
has been activated.
AUX GROUP: XM RADIO PAGE
62
XM Information Page
G500/600 Cockpit Reference Guide
190-00601-03 Rev G
XM® Radio Page (Optional)
Soft Keys Found on XM Radio Page
TO
AUX GROUP
AUX GROUP: XM RADIO PAGE
Selecting a Channel
1) While viewing the XM Radio page of the Aux Page Group, press the small
MFD knob and then turn the small MFD knob to highlight the desired
channel.
2) Press ENT to make the highlighted channel the Active Channel.
3) Press the small MFD knob to end editing.
4) Press CHNL and then the CH+ or CH- soft keys to increment up or down one
channel at a time in the active category.
5) Press CHNL and then the DIR CH soft key to directly select a channel in the
active channel field. Turn the small MFD knob and large MFD knob to select
desired channel.
6) Press ENT to save the selection or press the small MFD knob to cancel
selection.
Selecting a Channel within a Category
1) Press CATGRY to highlight the category window.
2) Press CAT+ or CAT- to cycle through the different categories or turn the small
MFD knob to the category and press ENT.
3) Turn the small MFD knob to move to the desired channel.
4) Press ENT to make that channel the active channel.
5) Press the small MFD to end editing.
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AUX GROUP
Volume
While viewing the XM Radio page of the Aux Group, press the
Press the
decrease radio volume. Press the small
the radio, press the
or the
VOL+
VOL+
or
or
MUTE
VOL-
VOL-
soft keys or turn the small
MFD
knob when done adjusting. To mute
MFD
soft key. To restore the radio volume, press
soft keys.
VOL
soft key.
knob to increase or
MUTE
Storing a Preset Channel
While viewing the XM Radio page, you may set a preset for the Active Channel.
Press the
PRESETS
soft key. Press and hold a preset soft key, such as
PS1
until it
blinks. You are able to preset up to 15 channels.
Recalling a Preset Channel
While viewing the XM Radio page, press the
preset soft key for the desired stored channel, such as
group of presets, press the
MORE
soft key.
PRESETS
PS1
soft key and press the
. To move to the next
again
AUX GROUP: XM RADIO PAGE
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Position Reporting Page
Soft Key Found on Position Reporting Page
AUX GROUP
AUX GROUP: POSITION REPORTING
Position Reporting Page
Position Reporting Status
The Status window shows the time until the next data transmission and the
status of the reporting system.
Settings Window
1) While viewing the Position Reporting page, press the small MFD knob.
2) Turn the large MFD knob to change the report type to either AFF (Automatic
Flight Following) or Standard.
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AUX GROUP
Status Window
Iridium® Phone Page (Optional)
Soft Keys Found on Iridium Phone Page
Name and
Phone
Number
Field
Volume Level
Phonebook
Catalog
Icon
AUX GROUP: IRIDIUM PHONE
Iridium Phone Page
For detailed use of the Iridium Phone system, see the latest revision of the
G500/600 Pilot’s Guide, P/N 190-00601-02.
Call Suppression
1) While viewing the Iridium Phone page, press the small MFD knob.
2) Turn the large MFD knob to select the Call Suppression type of Off, On,
or On During APR/MAPR/TERM. The last setting will suppress call during
approaches, missed approaches, or during terminal procedures.
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AUX GROUP
Creating Entries into Phonebook
1) While viewing the Iridium Phone page of the Aux Group, press the small MFD
knob to activate the cursor.
2) Turn the large MFD knob to highlight the phonebook catalog icon. Turn the
small MFD knob to display phonebook.
3) If the name already exists, it will be displayed in the drop down menu. If you
are adding a new entry, highlight, (New Entry). Press ENT.
4) Turn the small MFD knob to enter each letter of the name. Press ENT.
5) Turn the large MFD knob to move to enter the phone number. Turn the small
MFD to enter each number. Press ENT.
AUX GROUP: IRIDIUM PHONE
Deleting Entries into Phonebook
1) Press the small MFD knob to activate the cursor and then turn the large MFD
knob to select the Phone Book Catalog icon.
2) Turn the small MFD knob to display the contents of the Phone Book Catalog
and highlight the desired entry. Press ENT to select the catalog entry.
3) Turn the large MFD knob to highlight the DELETE key. Press ENT to delete
the catalog entry. Press the small MFD knob again to cancel the selection
cursor.
Editing a Phone Book Catalog Entry
1) Press the small MFD knob to activate the cursor and then turn the large MFD
knob to select the Phone Book Catalog icon.
2) Turn the small MFD knob to display the contents of the Phone Book Catalog
and highlight the desired entry. Press ENT to select the catalog entry.
3) Use the large MFD knob and small MFD knobs to make changes to the name
or number. Press ENT to save the changes. Press the small MFD knob again
to cancel the selection cursor.
Making a Phone Call
1) While viewing the Iridium Phone page, enter a phone number using the KEYS
soft key, rotary knobs, or select one from the Phone Book catalog.
2) Press the DIAL key.
3) After completing the call, press the HANG UP key.
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AUX GROUP
System Status Page
Soft Keys Found on System Status Page
The System Status page of the AUX Page group shows the status, serial number,
and version of LRUs as well as the effectivity information. There are no menu
options. In the LRU Status column, a green check means the unit is present and
operating properly, while a red X indicates an absence or failure.
System Status
1) While viewing the System Status page of the Aux Page Group, press the
AUX GROUP: SYSTEM STATUS PAGE
DB ACTV soft key and turn the small MFD knob to view the list of the
databases loaded into the GDU 620. Press the small MFD knob to exit.
2) Press the DB SYNC soft key synchronize databases with a second LRU.
Press the small MFD knob to exit.
3) Press the LRU soft key and turn the small MFD knob to scroll through the
status, serial number, and version of each LRU.
Press the small MFD knob to exit.
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Flight Plan Group
Active Flight Plan Page
Soft Keys Found on Active Flight Plan Page
Viewing Your Active Flight Plan
FPL GROUP
The active flight plan (as received from the active GPS unit) is shown on the
first page of the Flight Plan page group. No changes to the flight plan can be made
from the GDU 620. All flight plan changes must be made from the GPS unit.
FPL GROUP: ACTIVE FLIGHT PLAN
Active Flight Plan Page
1) While viewing the Active Flight Plan page of the FPL Page Group, press the
small MFD knob and then turn the large MFD knob to highlight waypoints in
the flight plan.
2) Press the INFO soft key to view information about the highlighted waypoint.
3) Press the small MFD knob to return to the Active Flight Plan page.
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FPL GROUP
WX/NOTAM
Waypoint Information Page
Soft Keys Found on Waypoint Information Page
Facility Identifier
Facility Name
Facility Location
Bearing & Distance
to Wpt from
Present Position
Map Orientation
Info/Map Soft Key
Rwy/Freq Soft Key
Airport Directory Soft Key
Waypoint Information Page
Facility Type
Map Region
Lat/Lon
Map Window
Wpt Weather
Info Soft Key
1) While viewing the Waypoint Information page of the FPL Page Group, press
the small MFD knob and then turn the small MFD knobs to enter or select
FPL GROUP: WAYPOINT INFO PAGE
the waypoint. You can also turn the small MFD knob counterclockwise to
obtain drop down menus for FPL, Nearest, and Recent.
2) Press the RWY/FREQ soft key to view runway and frequency information
about the waypoint.
3) Press the APT DIR soft key (if available) to view the airport directory
information such as facility hours, noise abatement, pattern, etc. Press the
small MFD knob and turn to scroll down the page (if available).
4) Press the WX or WX/NOTAM soft key (if available) to view METARs, TAFs, or
NOTAMs for the waypoint.
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Charts Page (Optional)
Soft Keys Found on Charts Page
Chart Information
FPL GROUP
FliteCharts
FliteCharts resemble the paper version of FAA published terminal procedures
®
FPL GROUP: CHARTS PAGE
charts. The charts are displayed with high-resolution and in color for applicable
charts. The database contains procedure charts for the United States only. This
database is updated on a 28-day cycle. FliteCharts is disabled 180 days after the
expiration date and is no longer available for viewing upon reaching the disable
date.
ChartView™ (Optional with Enablement Card)
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high resolution. The MFD depiction
shows the aircraft position on the moving map in the plan view of approach charts
and on airport diagrams. ChartView requires an enablement card.
The ChartView database is updated on a 14-day cycle. ChartView is disabled
70 days after the expiration date and is no longer available for viewing upon
reaching the disable date.
Selecting a Chart
1) While viewing the Charts page of the FPL Page Group, press the SELECT soft
key to change the airport or chart.
2) Turn the small and large MFD knobs to select the airport identifier and press
ENT to accept the selected airport.
3) Turn the large MFD knob to select the desired chart.
4) Press ENT to display the desired chart.
NOTE: The chart for the selected destination airport or approach is
automatically loaded. If no flight plan is entered, the chart page will
default to the nearest airport.
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FPL GROUP
Selecting Other Charts
You are able to choose other charts to display based on your flight plan (FPL),
charts of the nearest airport (NRST) or recently selected airports (RECENT).
1) While viewing the Charts page of the FPL Page Group, press the SELECT soft
key.
2) Turn the small MFD knob counterclockwise.
3) Turn the small MFD knob to show FPL, NRST, or RECENT.
4) Turn the large MFD knob to highlight the desired airport, then press ENT.
Display Charts From
Flight Plan
Display Charts Of
Nearest Airport
Display Charts From
Recent Choices
Viewing Charts and Panning
1) While viewing the Charts page of the FPL Page Group, press the RNG (Range)
keys to zoom in and out.
FPL GROUP: CHARTS PAGE
2) Press the small MFD knob to enter the panning mode and activate scroll bars
on the edges of the chart.
3) Turn the large MFD knob to move around the chart horizontally and turn the
small MFD knob to move vertically.
4) Press the small MFD knob to cancel the scroll bars and exit panning.
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FPL GROUP
Viewing Details of ChartView™ Charts
1) While viewing the Charts page of the FPL Page Group, press the DETAIL soft
key.
2) Press the HEADER, PLAN, PROFILE, or MINIMUMS soft keys to view
detailed sections for the chart for those topics.
Setting Minimums
1) While viewing the Charts page of the FPL Page Group, press the MENU key
to display the Options menu and press ENT.
2) Turn the small MFD knob to select the source, BARO or RAD ALT. Press the
ENT key.
3) Turn the small MFD knob to select the altitude. Press ENT to set the altitude.
Changing Day/Night View
1) While viewing the Charts page of the FPL Page Group, press the MENU key
to display the Options menu.
2) Turn the small MFD knob to Chart Setup. Press ENT. The Color Scheme
option will be highlighted.
3) Turn the small MFD knob to select Day - Auto - Night. Press the small MFD
knob to save the selected value and return to the Charts page.
4) If “Auto” is selected, turn the large MFD knob to highlight the Display Level
Brightness value. Turn the small MFD knob to change the display level value
for which the display will automatically switch from Day/Night brightness.
5) Press the MFD knob to save the selected value.
FPL GROUP: CHARTS PAGE
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FPL GROUP
Viewing NOTAMs (ChartView Only)
In the event there is an active NOTAM (Notice to Airmen) for a particular
chart, the
NOTAM
NOTAM
soft key.
soft key will be available. To view the information press the
FPL GROUP: CHARTS PAGE
74
Charts Page
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ALERTS
Alerts
Contact your Garmin dealer for service if any of the following alerts appear.
Refer to the Airplane Flight Manual and ADAS+ ETM documentation in the event
that Engine Trend Monitor (ETM) alerts are displayed.
On Screen Alerts
AlertDescription
ADC1 ALT EC
AHRS1 GPS
AHRS1/2 SRVC
AHRS1/2 TASAHRS1 or AHRS 2 is not receiving true airspeed from ADC.
ALT KEY INOPThe ALT key is disabled.
ALT NO COMPNo data from on or more altitude sensors.
ARINC 429 CONFIG ARINC 429 configuration error.
ARINC 708 CONFIG ARINC 708 configuration error.
AUD NOT AVAILAudio system is not available.
AUD SYS FAILAudio system has failed.
CAL LOSTRegistry reports that the GDU 620 has lost calibration data.
ADC Altitude Error Correction is unavailable.
GDC is reporting that altitude correction is unavailable.
AHRS 1 or AHRS 2 is not receiving any GPS information.
AHRS 1 or AHRS 2 is operating exclusively in no-GPS mode.
AHRS 1 or AHRS 2 is using the backup GPS information.
AHRS1 or AHRS 2 magnetic field model needs update. This
appears on the ground only.
ALERTS
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ALERTS
AlertDescription
• GDL 88 ADS-B Failure. Unable to transmit ADS-B messages.
• GDL 88 ADS-B fault.
• ADS-B fault: UAT receiver.
• ADS-B fault: 1090 receiver.
• GDL 88 needs service.
• GDL 88 ADS-B is not transmitting position. Check GPS
devices.
DATALINK
• GDL 88 control panel input fault. Check transponder mode.
• GDL 88 external traffic system inoperative or connection lost.
• GDL 88 configuration module needs service.
• GDL 88 is inoperative or connection to GDU is lost.
• GDL 88 CSA failure.
• GDL 88 external traffic system has a low battery.
ALERTS
• GDL 88 external traffic system in standby for more than 60
seconds.
DATA LOSTPilot stored data was lost. Recheck data and settings.
DB ERRDatabase found on top card.
DB SYNC COMPLETE
Database sync complete.
DB SYNC DISABLED No database card found to receive databases.
DB SYNC ERRORNot enough space to receive one or more databases.
DIAG MODESystem is in Diagnostic Mode.
DSCRT CONFIGDiscrete output configuration error.
ENG SENSOR UNIT
1/2
FAN 1/2 FAIL
• Configuration error. Communication with sensors is halted.
• Communication with sensors lost.
Cooling fan #1 or #2 has failed.
ETM CAPTUREADAS+ engine trend monitor is recording trend data.
ETM EXCEED
ADAS+ engine trend monitor is reporting an exceedence or
advisory condition.
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ALERTS
AlertDescription
ETM FAULTADAS+ engine trend monitor is reporting a system fault.
• Cooling fan 1/2 has failed.
• Unit may operate at extreme temperatures
FAN 1/2 FAIL
• Extended operation at high temperatures is not recommended
as damage to the GDU may occur.
• PFD/MFD coloration may be incorrect.
• Backlight may dim to reduce power and heat.
Gyro Emulation Type Mismatch Fault
Yaw Rate Scale Factor Mismatch Fault
GDU AHRS Monitor Fault
Pitch Deviation Fault
Roll Deviation Fault
Yaw Rate Deviation Fault
AHRS A429 Attitude Timeout Fault
AHRS A429 Attitude Invalid Fault
AHRS Pitch Out of Range Fault
AHRS Attitude Invalid Fault
GAD 43
AHRS A429 Heading Timeout Fault
AHRS A429 Heading Invalid Fault
Reference Timeout Fault
Application SCI Integrity Fault
Configuration Integrity Fault
AC Reference Lost
Calibration Integrity Fault
Unit Fault
Power Supply Fault
GAD 43 communication lost.
GAD 43E CONFIGGAD 43e configuration error. Communication halted.
GATE MODEAutomated testing is on.
GDL 69GDL 69/69A has failed.
ALERTS
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ALERTS
AlertDescription
GEO LIMITSAHRS too far North/South, no magnetic compass.
GPS1/2 FAILNo GPS1 or GPS2 data is available.
GPS(1/2) PPS FAILThe PPS signal has not been received in more than 5 seconds.
GSR FAILThe GSR 56 has failed.
GWX CONFIGGWX configuration error. Configuration service required.
GWX SERVICEGWX need service. Return unit for repair.
HDG FAULTAHRS 1 magnetometer fault has occurred.
HDG LOSTHDG features disabled or defaulted to GPS1 TRK.
• External HTAWS not available. Internal TERRAIN-HSVT
HTAWS
alerting enabled.
• External HTAWS configuration mismatch.
IAS NO COMPNo data from one or more airspeed sensors.
<LRU> CONFIG
Error in configuration of specific LRU, where <LRU> denotes
specific LRU.
<LRU> COOLINGSpecific LRU has poor cooling, reducing power usage.
<LRU> DB ERRDatabase for specific LRU is corrupt.
<LRU> KEYSTK<LRU> <KEY> is stuck.
ALERTS
<LRU> SERVICESpecific LRU needs service.
<LRU> VOLTAGE<LRU> has low voltage reducing power usage.
MANIFEST
GDU has received product data for an LRU that should have
a manifest entry, but is not in the manifest.
NAV1/2 FAILNo navigation receiver #1 or #2 data.
NO RADAR DATANo data is being sent to the GDU.
PIT NO COMPNo data from one or more pitch attitude sensors.
PREV EXCEED
RADAR CONTROLS
DISAGREE
ADAS+ engine trend monitor is reporting a previous
exceedence.
Data does not match for 15 seconds or more.
REGISTER GFDSData services are inoperative. GFDS is not registered.
ROL NO COMPNo data from one or more roll attitude sensors.
RS-232 CONFIGRS-232 configuration error.
RS-485 CONFIGRS-485 configuration error.
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AlertDescription
SIMULATORSim Mode is active. Do not use for navigation.
STORMSCOPEStormscope® either reports a failure or has timed out.
Out of available terrain region.
SVT DISABLED
Terrain DB resolution too low.
SW MISMATCHGDU software version strings to no match. Xtalk is off.
• External TAWS not available. Internal TERRAIN-SVT alerting
TAWS
enabled.
• External TAWS configuration mismatch.
TDBAirframe does not support terrain database.
TERRAIN DSP
Terrain awareness unavailable. (For configurations using
TAWS-B or TERRAIN-SVT).
TRAFFIC CONFIGADS-B traffic data does not match configuration.
• Traffic device has failed.
TRAFFIC FAIL
• Traffic data will no longer be displayed.
TRAFFIC STDBYTraffic device is in standby mode while airborne.
TRK LOSTGPS1 TRK lost. HSI defaulted to GPS2 TRK.
TRK TRAFFICHeading lost. Traffic is now based on track.
WX ALERTPossible severe weather ahead.
WX RADARWeather radar has failed.
WX RDR SERVICEWeather radar needs service.
WXR INPUT FAULTWeather radar is not receiving one or more inputs.
ALERTS
ALERTS
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ALERTS
TAWS-B Alerts
Alert Type
Excessive Descent Rate
Warning (EDR-W)
FLTA Terrain Warning
(RTC-W, ITI-W)
FLTA Obstacle Warning
(ROC-W, IOI-W)
FLTA Wire Warning
(ILI-W, RLC-W)
FLTA Terrain Caution
(RTC-C, ITI-C)
FLTA Obstacle Caution
(ROC-C, IOI-C)
PFD/MFD Alert
Annunciation
Aural Message
“Pull Up”
“Terrain Ahead, Pull Up; Terrain Ahead,
Pull Up”*
or
“Terrain, Terrain; Pull Up, Pull Up”
“
Obstacle Ahead, Pull Up; Obstacle Ahead,
Pull Up
”*
or
“
Obstacle, Obstacle; Pull Up, Pull Up
“
Wire Ahead, Pull Up; Wire Ahead, Pull Up
or
"Wire, Wire, Pull Up, Pull Up"
“Terrain Ahead; Terrain Ahead”*
or
“Caution, Terrain; Caution, Terrain”
“Obstacle Ahead; Obstacle Ahead”*
or
“Caution, Obstacle; Caution, Obstacle”
”
”*
ALERTS
FLTA Wire Caution
(ILI-C, RLC-C)
Premature Descent
Alert Caution (PDA)
Voice Callout
None
(VCO-500)
Excessive Descent Rate
Caution (EDR-C)
Negative Climb Rate
Caution (NCR-C)
* Alerts with multiple messages are configurable at installation and are installation-
dependent. Alerts for the default configuration are indicated with asterisks.
"Wire Ahead; Wire Ahead"
or
“Caution, Wire; Caution Wire”
“Too Low, Terrain”
“Five-Hundred”
“Sink Rate”
“Don’t Sink”*
or
“Too Low, Terrain”
\
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Terrain-SVT™ Alerts
ALERTS
Alert TypePFD/MFD Alert
Aural Message
Annunciation
GPS signal re-establishedNone“Terrain System Available”
Terrain System Test SuccessfulNone“Terrain System test OK”
Terrain System Test in ProgressNone
Terrain Alerting is disabledNone
No GPS position
Excessively degraded GPS
signal
Terrain SVT System Test Fail“Terrain System Failure”
Alert TypePFD/MFD Alert
“Terrain System Not Available”
Aural Message
Annunciation
FLTA Terrain Caution
(RTC-C, ITI-C)
FLTA Terrain Caution
(RLC-C, ILI-C)
FLTA Terrain Warning
(RTC-W, ITI-W)
FLTA Terrain Warning
(RLC-W, ILI-W)
FLTA Obstacle Caution
(ROC-C, IOI-C)
FLTA Obstacle Warning
(ROC-W, IOI-W)
“Caution, Terrain, Terrain”
“Caution, Wire, Wire”
“Warning, Terrain, Terrain”
“Warning, Wire, Wire”
“Caution, Obstacle, Obstacle”
“Warning, Obstacle, Obstacle”
ALERTS
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SYMBOLS
Map Page Symbols
SymbolDescription
Symbols
Unknown Airport
Non-towered, Non-serviced Airport
Towered, Non-serviced Airport
Non-towered, Serviced Airport
Towered, Serviced Airport
Soft Surface, Serviced Airport
Soft Surface, Non-serviced Airport
Private Airport
Heliport
SYMBOLS
82
Intersection
LOM (compass locator at outer marker)
NDB (Non-directional Radio Beacon)
VOR
VOR/DME
ILS/DME or DME-only
VORTAC
TACAN
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SafeTaxi® Symbols
SymbolDescription
Helipad
Airport Beacon
Under Construction Zones
Designated Water Areas
Traffic Symbols
TAS SymbolDescription
Other Traffic
SYMBOLS
SYMBOLS
Proximity Advisory (PA)
Traffic Advisory (TA)
Traffic Advisory Off Scale
TAS/TCAS Traffic Symbols
TIS SymbolDescription
Proximate Traffic (other than TA traffic)
Traffic Advisory (TA)
Traffic Advisory Off Scale
TIS Traffic Symbols
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SYMBOLS
SymbolDescription
,
Basic Non-Directional Traffic (White in Air, Brown on Ground)
Basic Directional Traffic (White in Air, Brown on Ground)
,
Basic Off-scale Selected Traffic
Proximate Non-Directional Traffic
Proximate Directional Traffic
Proximate Off-scale Selected Traffic
Non-Directional Alerted Traffic
Off-Scale Non-Directional Alerted Traffic
Directional Alerted Traffic
Off-Scale Directional Alerted Traffic
SYMBOLS
84
Non-Directional Surface Vehicle
Directional Surface Vehicle
ADS-B Traffic Symbols
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Terrain Obstacle Symbols
Threat Location
Unlighted Obstacle
Projected Flight Path
1000 ft
100 ft Threshold
Terrain more than 1000 ft below the aircraft altitude (Black)
Terrain between 100 ft and 1000 ft below the
aircraft altitude (Yellow)
Terrain above or
within 100 ft
below the aircraft
altitude (Red)
SYMBOLS
Unlighted Obstacle
(Height is less than
1000 ft AGL)
TowerWindmill
Lighted Obstacle
(Height is less
than 1000 ft AGL)
Unlighted Obstacle
(Height is greater
than 1000 ft AGL)
Grouped Obstacles
Lighted Obstacle
(Height is greater than
1000 ft AGL)
Power Line
The “*” notes
grouped obstacles.
NOTE: Obstacles will be removed from the Terrain/TAWS page when
range
(
RNG
)
exceeds 10 nm.
SYMBOLS
190-00601-03 Rev G
Terrain Altitude/Color Correlation
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SYMBOLS
Map Toolbar Symbols
SymbolDescription
Terrain Proximity Enabled and Available Indicator
Terrain Proximity Enabled and Not Available Indicator
Point Obstacle Enabled and Available Indicator
Point Obstacle Enabled and Not Available Indicator
Wire Obstacles Enabled and Available Indicator
Wire Obstacles Enabled and Not Available Indicator
StormScope
StormScope Enabled and Not Available Indicator
Traffic Enabled and Available Indicator
SYMBOLS
86
Traffic Enabled and Not Available Indicator
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SYMBOLS
XM® WX Weather Symbols and Product Age
The broadcast rate represents the interval at which XM WX Satellite Radio
broadcasts new signals that may or may not contain new weather data. It does
not represent the rate at which weather data is updated or new content is received
by the Data Link Receiver. Weather data is updated at intervals that are defined
and controlled by XM WX Satellite Radio and its data vendors. The product label
in the legend will turn yellow at half the expiration time and grey when expired.
Expired products will not be shown on the display.
Weather ProductExpiration Time
(Minutes)
NEXRAD (NEXRAD and Echo Top are Mutually Exclusive)30
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
(NEXRAD and Echo Top Mutually Exclusive)
Cloud Top (Cloud Top and Echo Top Mutually Exclusive)60
XM Lightning30
Cell Movement30
SIGMETs / AIRMETs60
METARs90
City Forecast90
Surface Analysis60
Freezing Levels120
Winds Aloft90
County Warnings60
PIREPS90
TFRs60
AIREPS90
Icing90
Turbulence180
Cyclone Warnings60
30
SYMBOLS
NOTE: Product age is not displayed for individual reports of AIRMETs,
SIGMETs, City Forecasts, County Warnings, Cell Movement and TFRs.
Product generation time is displayed for Freezing Level and Winds
Aloft instead of valid time.
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SYMBOLS
Miscellaneous Symbols
SymbolDescription
Low Wing Prop
High Wing Prop
Jet
Piston Rotorcraft
Turbine Rotorcraft
Default Map Cursor
Measuring Cursor
MFD Wind Vector (w/ valid GPS solution)
Parallel Track Waypoint
SYMBOLS
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88
Restricted/Prohibited/Warning/Alert
TFR (Temporary Flight Restrictions)
MOA
Class B Airspace (De-Emphasized Smart Airspace)
Class C Airspace (De-Emphasized Smart Airspace)
Class D Airspace (De-Emphasized Smart Airspace)