Except as expressly provided herein, no part of this manual may be reproduced, copied,
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without the express prior written consent 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 and to print one copy of this manual or of any
revision hereto, 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.
This manual reflects the operation of system software v2.00. Some differences in operation
may be observed when comparing the information in this manual to later software versions.
All other marks and logos are property of their respective owners. All rights reserved. Garmin
and SafeTaxi®are registered trademarks of Garmin International or its subsidiaries. Connext™,
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For information regarding the Aviation Limited Warranty, refer to Garmin’s website.
For aviation product support, visit flyGarmin.com.
SOFTWARE LICENSE AGREEMENT
BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN
("THE GARMIN PRODUCT"), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS OF
THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT
CAREFULLY. Garmin Ltd. and its subsidiaries ("Garmin") grants you a limited license to use the
software embedded in the Garmin Product (the "Software") in binary executable form in the
normal operation of the Garmin Product. Title, ownership rights, and intellectual property rights
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further acknowledge that the structure, organization, and code of the Software are valuable
trade secrets of Garmin and/or its third-party providers and that the Software in source code
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®
Page 3
Table of Contents
1 SYSTEM AT A GLANCE .....................................................................................................1-1
1.2 Unit Functions .......................................................................................... 1-4
Pilot Interface ........................................................................................................................................1-5
1.3 Unit Power ................................................................................................ 1-5
1.3.1 Instrument Test .................................................................................. 1-5
1.3.2 Power Off .......................................................................................... 1-5
Pilot Settings ........................................................................................................................................2-23
3.10 Active Flight Plan Map Overlay .............................................................. 3-34
3.11 GPS NAV Status Indicator Key ............................................................... 3-35
Direct To .................................................................................................................................................3-36
DO NOT USE TERRAIN AVOIDANCE DISPLAYS AS THE SOLE SOURCE OF INFORMATION
FOR MAINTAINING SEPARATION FROM TERRAIN AND OBSTACLES. GARMIN OBTAINS
TERRAIN AND OBSTACLE DATA FROM THIRD PARTY SOURCES AND CANNOT
INDEPENDENTLY VERIFY THE ACCURACY OF THE INFORMATION.
WARNING
DO NOT RELY SOLELY UPON TERRAIN PROXIMITY DATA FOR TERRAIN AVOIDANCE.
TERRAIN PROXIMITY IS NOT A CERTIFIED TERRAIN AWARENESS SYSTEM. IT IS AN AID
TO SITUATIONAL AWARENESS ONLY. USING TERRAIN PROXIMITY DATA DOES NOT
UNDER ANY CIRCUMSTANCES OR CONDITIONS RELIEVE THE PILOT’S RESPONSIBILITY
TO SEE AND AVOID TERRAIN OR OBSTACLES.
WARNING
ALWAYS REFER TO CURRENT AERONAUTICAL CHARTS AND NOTAMS FOR
VERIFICATION OF DISPLAYED AERONAUTICAL INFORMATION. DISPLAYED
AERONAUTICAL DATA MAY NOT INCORPORATE THE LATEST NOTAM INFORMATION.
WARNING
NEVER USE GPS ALTITUDE FOR VERTICAL NAVIGATION. THE ALTITUDE CALCULATED
BY GPS RECEIVERS IS GEOMETRIC HEIGHT ABOVE MEAN SEA LEVEL AND COULD VARY
SIGNIFICANTLY FROM THE ALTITUDE DISPLAYED BY PRESSURE ALTIMETERS (E.G., THE
OUTPUT FROM THE GDC 74A/B AIR DATA COMPUTER) OR OTHER ALTIMETERS IN THE
AIRCRAFT. ALWAYS REFER TO THE PRESSURE ALTIMETERS IN THE AIRCRAFT FOR
CURRENT PRESSURE ALTITUDE.
WARNING
NEVER USE EXPIRED DATABASES. UPDATE DATABASES REGULARLY TO ENSURE
CURRENCY. USE OUT OF DATE DATABASE INFORMATION AT YOUR OWN RISK.
WARNING
NEVER USE BASEMAP INFORMATION (LAND AND WATER DATA) AS THE SOLE MEANS
OF NAVIGATION. BASEMAP DATA IS INTENDED ONLY TO SUPPLEMENT OTHER
APPROVED NAVIGATION DATA SOURCES AND SHOULD BE CONSIDERED ONLY AN AID
TO ENHANCE SITUATIONAL AWARENESS.
WARNING
DO NOT RELY SOLELY UPON THE DISPLAY OF TRAFFIC INFORMATION TO
ACCURATELY DEPICT ALL OF THE TRAFFIC WITHIN RANGE OF THE AIRCRAFT. DUE TO
LACK OF EQUIPMENT, POOR SIGNAL RECEPTION, AND/OR INACCURATE
INFORMATION FROM AIRCRAFT OR GROUND STATIONS, TRAFFIC MAY BE PRESENT
THAT IS NOT REPRESENTED ON THE DISPLAY.
190-02207-02 Rev. 1GPS 175/GNX 375 Pilot’s Guide
vii
Page 10
Warnings, Cautions, and Notes
WARNING
NEVER USE DATALINK WEATHER INFORMATION FOR MANEUVERING IN, NEAR, OR
AROUND AREAS OF HAZARDOUS WEATHER. INFORMATION CONTAINED WITHIN
DATALINK WEATHER PRODUCTS MAY NOT ACCURATELY DEPICT CURRENT WEATHER
CONDITIONS.
WARNING
DO NOT USE THE INDICATED DATALINK WEATHER PRODUCT AGE TO DETERMINE
THE AGE OF THE WEATHER INFORMATION SHOWN BY THE DATALINK WEATHER
PRODUCT. DUE TO TIME DELAYS INHERENT IN GATHERING AND PROCESSING
WEATHER DATA FOR DATALINK TRANSMISSION, THE WEATHER INFORMATION
SHOWN BY THE DATALINK WEATHER PRODUCT MAY BE OLDER THAN THE
INDICATED WEATHER PRODUCT AGE.
WARNING
ALWAYS REFER TO CURRENT AERONAUTICAL CHARTS FOR APPROPRIATE MINIMUM
CLEARANCE ALTITUDES. THE DISPLAYED MSAs ARE ONLY ADVISORY IN NATURE AND
SHOULD NOT BE RELIED UPON AS THE SOLE SOURCE OF OBSTACLE AND TERRAIN
AVOIDANCE INFORMATION.
WARNING
DO NOT USE GPS TO NAVIGATE TO ANY ACTIVE WAYPOINT IDENTIFIED AS A “NON
WGS84 WPT” BY A SYSTEM MESSAGE. “NON WGS84 WPT” WAYPOINTS ARE DERIVED
FROM AN UNKNOWN MAP REFERENCE DATUM THAT MAY BE INCOMPATIBLE WITH
THE MAP REFERENCE DATUM USED BY GPS (KNOWN AS WGS84) AND MAY BE
POSITIONED IN ERROR AS DISPLAYED.
viii
WARNING
DO NOT RELY SOLELY UPON THE DISPLAY OF TRAFFIC INFORMATION FOR COLLISION
AVOIDANCE MANEUVERING. THE TRAFFIC DISPLAY DOES NOT PROVIDE COLLISION
AVOIDANCE RESOLUTION ADVISORIES AND DOES NOT UNDER ANY CIRCUMSTANCES
OR CONDITIONS RELIEVE THE PILOT’S RESPONSIBILITY TO SEE AND AVOID OTHER
AIRCRAFT.
WARNING
DO NOT RELY ON THE ACCURACY OF ATTITUDE AND HEADING INDICATIONS IN
GEOGRAPHIC AREAS WHERE VARIATION IN THE EARTH’S MAGNETIC FIELD EXISTS.
THIS INCLUDES: NORTH OF 72° NORTH LATITUDE AT ALL LONGITUDES; SOUTH OF 70°
SOUTH LATITUDE AT ALL LONGITUDES; NORTH OF 65° NORTH LATITUDE BETWEEN
LONGITUDE 75° W. AND 120° W. (NORTHERN CANADA); NORTH OF 70° NORTH
LATITUDE BETWEEN LONGITUDE 70° W. AND 128° W. (NORTHERN CANADA); NORTH
OF 70° NORTH LATITUDE BETWEEN LONGITUDE 85° E. AND 114° E. (NORTHERN
RUSSIA); SOUTH OF 55° SOUTH LATITUDE BETWEEN LONGITUDE 120° E. AND 165° E.
(REGION SOUTH OF AUSTRALIA AND NEW ZEALAND).
GPS 175/GNX 375 Pilot’s Guide190-02207-02 Rev. 1
Page 11
Warnings, Cautions, and Notes
WARNING
DO NOT RELY SOLELY UPON DATALINK SERVICES TO PROVIDE TFR INFORMATION.
ALWAYS CONFIRM TFR INFORMATION THROUGH OFFICIAL SOURCES SUCH AS
FLIGHT SERVICE STATIONS OR AIR TRAFFIC CONTROL.
WARNING
DO NOT LEARN OPERATIONAL PROCEDURES IN THE AIR. FOR SAFETY REASONS,
THOROUGHLY PRACTICE BASIC OPERATION ON THE GROUND BEFORE ACTUAL USE.
WARNING
REVIEW AND UNDERSTAND ALL ASPECTS OF THIS PILOT’S GUIDE. DOING SO REDUCES
THE RISK OF UNSAFE OPERATION.
WARNING
ALWAYS RESOLVE ANY DISCREPANCIES BETWEEN THE DISPLAY AND OTHER
NAVIGATION SOURCES WHEN THEY OCCUR. DURING FLIGHT OPERATIONS,
COMPARE DISPLAY INDICATIONS TO INFORMATION FROM OTHER NAVAIDS, VISUAL
SIGHTINGS, CHARTS, AND OTHER AVAILABLE SOURCES BEFORE CONTINUING
NAVIGATION.
CAUTION
DO NOT CLEAN DISPLAY SURFACES WITH ABRASIVE CLOTHS OR CLEANERS
CONTAINING AMMONIA. THEY WILL HARM THE ANTI-REFLECTIVE COATING.
CAUTION
ENSURE THAT ANY UNIT REPAIRS ARE MADE BY AN AUTHORIZED GARMIN
SERVICE CENTER. UNAUTHORIZED REPAIRS OR MODIFICATIONS COULD VOID
BOTH THE WARRANTY AND AFFECT THE AIRWORTHINESS OF THE AIRCRAFT.
NOTE
All visual depictions contained within this document, including screen images
of the system panel and displays, are subject to change and may not reflect
the most current system and aviation databases. Depictions of equipment
may differ slightly from the actual equipment.
NOTE
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 system utilize GPS as a precision electronic
NAVAID. Therefore, as with all NAVAIDs, information presented by the
system can be misused or misinterpreted and, therefore, become unsafe.
190-02207-02 Rev. 1GPS 175/GNX 375 Pilot’s Guide
ix
Page 12
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
Interference from GPS repeaters operating inside nearby hangars can cause
an intermittent loss of attitude and heading displays while the aircraft is on
the ground. Moving the aircraft more than 100 yards away from the source
of the interference should alleviate the condition.
NOTE
Use of polarized eye wear may cause the flight displays to appear dim or
blank.
NOTE
This product, its packaging, and its components contain chemicals known to
the State of California to cause cancer, birth defects, or reproductive harm.
This notice is being provided in accordance with California’s Proposition 65.
If you have any questions or would like additional information, please refer
to our website at www.garmin.com/prop65.
NOTE
Operating the system in the vicinity of metal buildings, metal structures, or
electromagnetic fields can cause sensor differences that may result in
nuisance miscompare annunciations during start up, shut down, or while
taxiing. If one or more of the sensed values are unavailable, the annunciation
indicates no comparison is possible.
NOTE
The system responds to a terminal procedure based on data coded within
that procedure in the Navigation Database. Differences in system operation
may be observed among similar types of procedures due to differences in the
Navigation Database coding specific to each procedure.
NOTE
Do not use SafeTaxi functions as the basis for ground maneuvering. SafeTaxi
functions do not comply with the requirements of AC 120-76C and are not
qualified for use as an airport moving map display. SafeTaxi is to be used for
orientation purposes only.
xGPS 175/GNX 375 Pilot’s Guide190-02207-02 Rev. 1
Page 13
Warnings, Cautions, and Notes
NOTE
The FAA has asked Garmin to remind pilots who fly with Garmin
database-dependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and
advisory guidance and information related to the use of databases in the
National Airspace System.
• Garmin equipment will only recognize and use databases that are obtained
from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen that
have a Type 2 LOA from the FAA are assured compliance with all data quality
requirements (DQRs). A copy of the Type 2 LOA is available for each
applicable database and can be viewed at flyGarmin.com by selecting
“Aviation Database Declarations.”
• Use of a current Garmin or Jeppesen database in
is required for compliance with established FAA regulatory guidance, but
does not constitute authorization to fly any and all terminal procedures that
may be presented by the system. It is the pilot’s responsibility to operate in
accordance with established AFM(S) and regulatory guidance or limitations
as applicable to the pilot, the aircraft, and installed equipment.
your Garmin equipment
NOTE
The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at flyGarmin.com by
selecting “Database Exclusions List.”
NOTE
The pilot/operator must have access to Garmin and Jeppesen database alerts
and consider their impact on the intended aircraft operation. The database
alerts can be viewed at flyGarmin.com by selecting “Aviation Database
Alerts.”
NOTE
If the pilot/operator wants or needs to adjust the database, contact Garmin
Product Support.
NOTE
Garmin requests the flight crew report any observed discrepancies related to
database information. These discrepancies could come in the form of an
incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any
other displayed item used for navigation or communication in the air or on
the ground. Visit flyGarmin.com and select “Aviation Data Error Report.”
The navigation databases used in Garmin navigation systems contain Special
Procedures. Prior to flying these procedures, pilots must have specific FAA
authorization, training, and possession of the corresponding current, and
legitimately-sourced chart (approach plate, etc.). Inclusion of the Special
Procedure in the navigation database DOES NOT imply specific FAA
authorization to fly the procedure.
AC 90-100A Statement of Compliance
The Garmin navigational unit meets the performance and functional requirements of
FAA Advisory Circular (AC) 90-100A, U.S. Terminal and En Route Area Navigation(RNAV) Operations.
xii
GPS 175/GNX 375 Pilot’s Guide190-02207-02 Rev. 1
Page 15
Record of Revision
REVISIONDATECHANGE DESCRIPTION
102/07/19Experimental Release.
Layout
About This Guide
SECTIONTITLE
1
2
3
4
5
6
7
8
System at a Glance
Get Started
Navigation
Planning
Hazard Awareness
Messages
Qualification
Glossary
The design and layout of this guide is
intended to provide clear, concise
sections written in the logical order
of a pilot’s flight instrument and
systems scan.
Electronic Document Features
Versions of this guide are saved in Adobe Acrobat and are available for download at:
The GPS 175 and GNX 375 are the first 2” by 6.25” panel mount navigators to
employ full color capacitive touchscreen technology.
The GPS 175 is a TSO-C146e compliant GPS/WAAS navigator with en route,
terminal, and precision/non-precision approach capabilities. The GNX 375 combines
the functionality of the GPS 175 with a TSO-C112e (Level 2els, Class 1) compliant
mode S transponder.
Each unit is Bluetooth compatible, providing flight plan, traffic, weather, and
position data to an available portable electronic device.
GPS 175 NAVIGATOR
• TSO-C146e compliant GPS/WAAS navigator and internal GPS source
• TSO-C195b (Class B1, B3, B5, B7) compliant with an active ADS-B In source
• Certified compatible with ADS-B Out 2020 mandate
[1] Function availability dependent upon aircraft interfaces or enablement.
[2] ADS-B In via 1090 MHz (traffic) and 978 MHz UAT (traffic and weather).
[3] Requires Wi-Fi connection via Flight Stream 510.
The unit receives power directly from the aircraft’s electrical system. Upon power-up,
the bezel key backlight momentarily illuminates. System failure annunciations
typically disappear within the first 30 seconds after power-up.
The start-up screen presents the unit software versions, the name and status of all
installed databases, and the Database Updates page access key. These features are
available only at power up.
Tapping Continue advances to the Instrument Test page.
If an instrument remains flagged after one minute, check the status of the
associated LRU, then contact a Garmin dealer for support.
1.3.1Instrument Test
To ensure safe operation, continuous built-in test features exercise the unit’s
processor, memory, external inputs, and outputs. The Instrument Test page displays
the results of all external equipment checks performed by the unit.
Review this list to ensure that all
CDI outputs and other displayed
data are correct for the
connected equipment.
1.3.2Power Off
WARNING
NEVER ATTEMPT TO POWER OFF THE UNIT WHILE AIRBORNE UNLESS
OPERATIONAL PROCEDURES DICTATE.
Pushing and holding the Power key for
0.5 seconds initiates the power off sequence.
Shutdown occurs once the timer reaches zero.
Power off annunciation temporarily replaces
the knob function indicator.
Certain momentary controls (e.g., directional arrow
keys) provide a secondary tap and hold function.
Tap the key and hold your finger in place until the
desired action occurs.
Use this gesture for:
• Scrolling with arrow keys
• Increasing/decreasing values continuously
A smooth motion that involves touching an object,
then sliding your finger across the screen and then
lifting up.
Use this gesture for:
• Accessing multiple panes (right or left swipes)
• Viewing and scrolling lists
• Panning across a map display
Swiping the screen in a quick upward or downward
motion. Information moves at a fast speed, then slows
to a stop.
Touch any map with two fingers at the same time,
then bring the fingers close together (pinch) or spread
them apart (stretch). Just remember: stretch to zoom
in and pinch to zoom out.
Use this gesture for:
• Magnifying map features
Page 24
System at a Glance
1.5.1Keys
COMMON COMMANDS
Open the system messages
list. A flashing icon indicates
unread messages.
Open a context menu.Input a specified value.
Return to the previous
page.
Cancel an active function
without inputting data.
Select the corresponding
item (e.g., database
update). A checkmark
confirms selection.
FUNCTION KEYS
Toggle keys turn a specific function on or off.
The current state of the function is indicated
below the key label.
On
Off
PAGE ICONS
Tapping one of these icons opens the corresponding page. Menu pages provide
additional icons for accessing functions on subpages.
Menus group related controls into an expandable pane, allowing access to multiple
functions on a single page. Depending on the number of available functions, a menu
may comprise more than one pane.
Multiple panes are accessible by
way of swipe or inner knob turn.
Active Pane
An indicator at the bottom of the menu shows
which pane is active.
POP-UP MENUS
Pop-up menus open to the default
or previously selected value.
Underlying Page Hidden
Default or Current Setting
LISTS
Scrollable lists group control keys related to a single function (e.g., FIS-B Weather).
When scrolling, all keys in the list are inactive.
Toggle keys either enable or disable list items.
In some cases, Settings or Range keys provide
access to selectable setting options.
Inner and outer control knobs offer an alternative method for
selecting and modifying data without the use of touch keys.
OuterInner
KNOB FUNCTIONS
• Selecting reference controls
Outer Knob
Inner Knob
(Turn)
• Selecting a page shortcut
• Cursor placement and initial field/page selections
• Moving cursor forward or backward within data field
• Zooming
• Selecting reference values
• Inputting data
• Modifying individual characters in data entry field
System at a Glance
Inner Knob
(Push)
• Entering current or specified numerical value
• Toggling Map page user fields on or off
• Accessing the Direct To function from the Home page
1.6.1Knob Function Indicators
A locater bar works in conjunction with the outer knob providing quick access to the
indicated page. Turning the outer knob clockwise or counter-clockwise moves the
locater through displayed menu options.
Active
Page
Slot 1
(Map)
Available Knob
Function
Slot 3
Slot 2
Slot 1 is a dedicated Map
page shortcut. Slots 2 and 3
are customizable. Selectable
page options are dependent
upon configuration.
The active page name
displays in cyan.
Additional icons located to
the right of the bar indicate
available knob functions for
the associated page (e.g.,
zoom, numeric entry).
Save images to an SD card at any time using a screen capture. Images automatically
save to the “print” folder in the SD card root directory.
1.Insert an SD card into the card slot.
2.Push and hold the control knob.
3.With knob depressed, push and release the Home/Power key.
A camera icon momentarily shows in the annunciator bar indicating a successful
screen capture. To view saved images, remove the SD card and open the “print”
folder on a computer.
GDL 88/GTX 345 ADS-B transceiver
(applicable to GPS 175 only)
The system consists of multiple LRUs,
which are installed behind the
instrument panel or in a separate
avionics bay. Their modular design
aids system maintenance and unit
replacement.
Optional LRUs may include
compatible equipment from either
Garmin or a third party manufacturer.
Some LRUs provide features that
require registration and/or
enablement prior to activation.
The ADC and AHRS sense air data and aircraft attitude for display and use by other
systems. AHRS units have a magnetometer interface for determining magnetic
heading. ADC units have an OAT probe interface for measuring outside air
temperature.
The navigator uses two types of databases: active and standby. Active databases are
in use by the system. Standby databases have not reached the effective date. During
normal operation, information about all active and standby databases are viewable
on the associated info page.
From the Home page, tap System > System Status > Select Active or Standby.
DB INFO PAGEDISPLAYS
Active
Standby• Information about databases that are not yet effective
• Information about databases currently in use
• View Copyrights key
The Standby DB Info page notifies when
no standby databases are available.
VIEW COPYRIGHTS
Tapping this key displays copyright information for all
installed databases.
• A newer database is detected on the SD card or in the
internal standby queue
• A newer database is within its effective dates
• The aircraft is on ground
When a newer database is available, follow the on-screen prompts to complete the
update process.
A status page displays a progress bar and the name of each database as it uploads to
the unit. Terrain databases may require up to 5 minutes for transfer. Total transfer
time depends on the SD card type.
The unit automatically restarts once the update is complete. The update is indicated
in the list of currently installed databases.
INSTALL OR UPDATE A DATABASE USING AN SD CARD
1. Download a database onto an SD card.
2. Insert the SD card with the most recent database(s) into the card slot.
3. Power on the unit.
Selecting Update opens the DB Updates page.
A list displays the newest databases.
All newer databases (effective and expired)
transfer from the SD card to the internal
standby queue.
BASEMAP AND TERRAIN UPDATES
These databases automatically transfer from an SD card without any prompting or
progress indications. They do not require pilot confirmation or a unit restart.
Database Concierge allows wireless transfer of databases
from a mobile device.
A pilot selects and downloads databases inside the Garmin
Pilot app. Transfers occur once Flight Stream 510 establishes a
wireless connection inside the aircraft.
DATABASE CONCIERGE TRANSFER FUNCTIONS
• Automatic updates for databases with effective dates
• Preloads databases that are not yet effective by placing them in the internal
standby queue
• Displays database type, cycle, effective date, and transfer progress
• Start key for manual operation
• Pilot confirmation required
TRANSFER A DATABASE USING DATABASE CONCIERGE
1. Purchase database(s) from flyGarmin.com.
2. Open Garmin Pilot and follow the download instructions.
3. Install Flight Stream 510 and then power on unit.
Database Concierge transfers
databases from the app to
Flight Stream 510.
A progress bar shows when this
process is complete.
Database Transfer Status
The unit either updates or
preloads databases based on
their effective date. A second
progress bar indicates upload
Database Update Status
Tapping Skip cancels any unfinished wireless transfers and
initiates the update process.
The unit activates any databases that completed transfer before the interruption.
Previously selected databases on an SD card or in the internal standby update as well.
The message “Transfers interrupted” displays if no databases are available.
status. The unit automatically
restarts upon database activation.
• Unit allows pairing of up to 13 Bluetooth devices, with two simultaneous
device connections
• Auto reconnect function is not available for Android devices
2.6Connext Setup
Connext works via the Bluetooth data link to
provide up-to-date, wireless information
throughout the cockpit.
The Connext interface allows communication with applications (i.e., Garmin Pilot
and ForeFlight Mobile) while running on a portable electronic device.
Connext Features
The following features are available on your portable electronic device.
• GPS position and velocity information [1] [2]
• ADS-B In traffic data [1]
• FIS-B weather and flight information [2]
• Uncorrected barometric pressure altitude used by transponder and ADS-B [1]
• AHRS data via Connext and a built-in sensor [2] [3]
[1] GNX 375 only.
[2] External ADS-B In device required for GPS 175.
[3] Occurs when GNX 375 is installed as a standalone device. Attitude data does not output to
other installed avionics.
[4] The internal AHRS sensor is only for use with a portable electronic device. All internal AHRS
functions are automatic and do not require pilot action.
Tapping Mode opens a menu of the available transponder
modes. Options include Standby, On, and Altitude Reporting.
MODEFUNCTION
• Transponder does not reply to interrogations or
transmit ADS-B Out
Standby
On
Altitude
Reporting
• Bluetooth functions remain operational
• Unit continues to receive ADS-B In information, but is
not a TIS-B participant
• Transponder replies to interrogations. Replies do not
include pressure altitude
• Reply (R) symbol on the display indicates the
transponder is responding
• Transponder replies to identification and altitude
interrogations
• Reply (R) symbol indicates the transponder is
responding
• GNX 375 transmissions include pressure altitude
Get Started
During Altitude Reporting mode, all aircraft air/ground state transmissions are
handled via the transponder and require no pilot action. Always use this mode
while in the air and on the ground, unless otherwise requested by ATC.
Tapping this key activates the
IDENT function for 18 seconds.
This signal distinguishes the
transponder from others on
the air traffic controller’s
screen.
Page 53
TRANSPONDER STATUS INDICATIONS
IDENTStandby Mode
Get Started
• Reply active
• Identify function active
• No change to
transponder code
IDENT with New Squawk CodeAltitude Reporting Mode
• Reply active
• Transponder code
modified
• Standby mode
• Current squawk code
(inactive)
• Altitude reporting mode
• Reply active
• Identify function active
• VFR squawk code
(active)
SYMBOLMEANING
Reply active
Identify function active
Transponder in operation
Altitude Reporting
Standby
Press to initiate the IDENT function (code unmodified)
Press to accept modified code and initiate IDENT function
Transponder functions are controllable from a connected G3X Touch display.
Control features include:
• Squawk code• Transponder mode
• IDENT• ADS-B transmission
• Flight ID
For transponder control operation, consult the G3X Touch Pilot’s Guide.
2.13XPDR Alert
If the transponder fails:
• Red “X” displays over the IDENT key
• Advisory message alerts
• XPDR control page is not available
Transponder fail annunciations are designed to be immediately recognizable.
If a failure occurs while the control page is active, the display automatically returns
to the previous page.
UNITCONDITION
GPS 175GDL 88 failure.
GNX 375ADS-B interboard communication failure.
For information regarding pilot response to a transponder failure, consult the
AFMS.
Other setup options allow
you to monitor time in flight
and create custom reminder
messages. These reside in the
system Utilities.
Set the scale for the course deviation indicator.
Scale values represent full scale deflection for the
CDI to either side.
Options: • 0.30 nm • 1.00 nm • 2.00 nm • Auto
By default, the scale is set to “Auto.” At this setting, the CDI scale is set to 2.0 nm
during the en route phase of flight.
Within 31 NM (terminal area) of your destination airport, the CDI scale linearly ramps
down to 1.0 NM over a distance of 1 NM.
Likewise, when leaving your departure airport the CDI scale is set to 1.0 NM and
gradually ramps up to 2 NM beyond 30 NM (from the departure airport). During GPS
approach operations the CDI scale gradually transitions down to an angular CDI
scale.
At 2.0 NM before the final approach fix (FAF), CDI scaling is tightened from 1.0 NM
to the angular full scale deflection (typically the angular full-scale deflection is 2.0°,
but will be as defined for the approach)
If a lower CDI scale setting is selected (i.e., 1.0 or 0.3 NM), the higher scale settings
are not selected during ANY phase of flight. For example, if 1.0 NM is selected, the
unit uses this for en route and terminal phases and ramps down further during an
approach.
Horizontal alarm limits (HAL) follow the selected CDI scale, unless the corresponding
flight phase requires a lower alarm limit. For example, the selected scale setting is
1.0 nm, but full-scale deflection during approach still follows the approach scale
setting (0.30 nm).
FLIGHT
PHASE
Approach0.30 nm or Auto0.30 nm
Terminal1.00 nm or Auto
En Route2.00 nm or Auto
OceanicAuto
CDI SCALE
HORIZONTAL
ALARM LIMIT
1.00 nm
2.00 nm
2.00 nm
2.14.2CDI On Screen
Toggling this setting displays the CDI scale on screen. When active, a CDI with lateral
deviation indicator displays below the GPS NAV Status Indicator key.
CDI OFFCDI ON
Only the Flight Plan page
access key is available.
The CDI provides no indications
without an active flight plan.
Airspace alerts generate a message and filtering of the Nearest
Airspace list. They rely on three-dimensional data (altitude,
latitude, and longitude) to avoid nuisance alerts.
FEATURE LIMITATIONS
• Alert altitudes are dependent on aircraft and airspace altitudes and the
pilot-specified altitude buffer value
Control keys allow you to select which airspace boundaries
generate an alert annunciation upon entry.
Alert boundaries for controlled airspace are
sectorized to provide complete information
on any nearby airspace.
Alert settings do not alter the depiction of
airspace, nor do they change Smart Airspace
settings on the Map page.
With the exception of Altitude Buffer,
airspace alert options are on/off only.
Airspace alerts for Prohibited airspace
cannot be disabled.
Depending on configuration, display brightness is controlled using
inputs from the built in photocell, aircraft dimmer bus, or both.
2.20.1Automatic Brightness Control
Dimming is limited to prevent on screen indications from becoming unreadable. The
built in photocell automatically controls display brightness based on ambient light
levels.
Backlight
Intensity Level
Manual Offset
Indicator
During automatic control, the pilot
may still adjust brightness using
the manual offset controls in the
Backlight page.
The unit retains manual offset
settings over power cycles.
Decrease
Backlight
Increase
Backlight
2.20.2Manual Brightness Control
Optionally, the unit is configurable to use an aircraft dimming bus for display
brightness control. Upon reaching minimum input level, display brightness reverts to
the photocell. This prevents the display from going black in the event of a dimmer
input failure.
Installer configured curves determine the amount of change in brightness that
occurs in response to a control adjustment.
If brightness control is not satisfactory, contact a Garmin dealer to adjust the
lighting curves.
The unit generates annunciations in response to various conditions that may occur.
These abbreviated messages are grouped according to the level of urgency and
required response. They display in order of priority, from highest to lowest.
1. Warnings
2. Cautions
3. Mode & function advisories
WARNINGS & CAUTIONS
Warnings require immediate attention. Cautions indicate the presence of an
abnormal condition that may require pilot action. A warning may follow a caution if
no attempt is made to correct the condition (e.g., altering the aircraft’s path toward
the alerted terrain or obstacle).
MODE & FUNCTION ADVISORIES
Advisories provide status and operating information.
System advisories display on a dedicated page or slide over window. Depending on
the number of advisories, this list may be scrollable.
Function or mode specific advisories appear as unobstructed annunciations on the
associated display.
Alert annunciations are abbreviated messages that indicate an alerted function or
mode. The color of the annunciation depends on the alert type.
ALERT COLORS
WARNING
CAUTION
ADVISORY
When an alert is triggered, the annunciation flashes by alternating text and
background colors. It turns solid after five seconds. All annunciations remain active
(solid) until the condition is resolved or no longer a threat.
ANNUNCIATION LOCATION
Alerts and informational advisories annunciate in the annunciator bar along the
bottom of the screen.
If a warning or caution relating to terrain or traffic occurs, a pop-up window may
display. These pop-ups only appear if the alerted function’s associated page is not
active.
POP-UP ALERT PRIORITY
In the event of simultaneous
alerts, pop-up windows display in
the following order:
1. Terrain alerts
2. Traffic alerts
1Threat Indication4Alert Inhibit Key
2Alert Annunciation5Go to <Page> Key
Each pop-up alert provides:
• Threat indication
• Alert annunciation
• Option to inhibit or mute the alert
• Control for closing the pop-up window
• Direct access to the associated page
Pop-up Alert Layout
3Close Pop-up Window Key
To open the indicated page, tap Go to <Page>.
To acknowledge the alert and return to previous page view, tap Close.
2.22.3Aural Alerts
FEATURE LIMITATIONS
• GNX 375 only (traffic alerts)
Traffic alerts are accompanied by an aural voice message. Voice gender is configured
during installation.
Each bar is labeled with the SVID
of the corresponding satellite.
Numbers vary according to
satellite type.
• GPS:1to31
• SBAS: 120 to 138
A graph shows GPS signal strength for up
to 15 satellites. As the GPS receiver locks
onto satellites, a signal strength bar appears
for each satellite in view.
Graph symbols depict the progress of
satellite acquisition. Some data may not
display until the unit has acquired enough
satellites for a fix.
SYMBOLCONDITION
Not presentReceiver is searching for the indicated satellites.
Gray bar, empty
Gray bar, solid
Yellow bar, solid
Cyan bar,
cross-hatch
Cyan bar, solid
Green bar, solid
D (inside bar)
Satellite located.
Satellite located, receiver is collecting data.
Data collected, but satellite is excluded from position
solution (i.e., it is not in use).
Satellite located, but FDE excludes it for being a faulty
satellite.
Data collected, but receiver is not using satellite in the
position solution.
Data collected, satellite in use in the current position
solution.
EPU is the horizontal position error estimated by the
fault detection and exclusion algorithm, in feet or
meters.
Information fields indicate the
accuracy of the position fix.
HFOM and VFOM values
represent 95% confidence levels
in horizontal and vertical
accuracy.
Lower values mean higher
accuracy. Higher values are the
least accurate.
FDE PREDICTION
NOTE
Under FAR parts 91, 121, 125, and 135, FDE must be used prior to all
oceanic or remote area flights using the GPS 175/GNX 375 as a primary
means of navigation.
This program uses an algorithm to predict FDE availability. If the unit has not been in
operation for more than six months, acquiring satellite data to establish almanac and
satellite orbit information may take 5 to 10 minutes.
2.24.1Circle of Uncertainty
FEATURE LIMITATIONS
• Available only when the aircraft is on ground
• Displays only on the Map page
• Depicts area surrounding the ownship when GPS
cannot accurately determine aircraft location
• Expands as GPS horizontal accuracy degrades
• Shrinks as accuracy improves
• Transparent so as not to obstruct other features
Operating with SBAS active outside of the service area may cause elevated
EPU values to display on the status page. Regardless of the EPU value
displayed, the LOI annunciation is the controlling indication for
determining the integrity of the GPS navigation solution.
SBAS supports wide area or regional augmentation through the
use of additional satellite broadcast messages.
Tap this key and select from the list of providers.
PROVIDERSERVICE AREAS
EGNOSMost of Europe and parts of North Africa.
GAGAN
MSAS
WAAS
India
Japan only.
Alaska, Canada, the 48 contiguous states,
and most of Central America.
2.24.3GPS Status Annunciations
Once the GPS receiver determines the aircraft’s position, the unit displays position,
altitude, track, and ground speed data. GPS status annunciates under the following
conditions.
ANNUNCIATIONCONDITION
GPS receiver uses last known position and satellite orbital
A logging function stores WAAS diagnostic data in the unit’s
internal memory. This information is available for export to an
SD card for later analysis.
FEATURE REQUIREMENTS
• SD card
The export function resides in the Logs page.
This function is not available if no log files are present.
WAAS Diagnostic Log Functions
• Generates log files automatically upon unit power-up
• Provides WAAS engine data in the form of serial text messages
• Overwrites oldest file when the internal log reaches capacity
• Exports to the “log_files” folder on the SD card
Land and water data are for general reference only. Data accuracy is not suitable for
use as a primary navigation source. The information is intended to supplement and
not replace official government charts and notices.
DATA DRAWING ORDER
The electronic map draws data in order of priority, from highest (1) to lowest (39),
with higher priority features drawn atop those of lower priority.
Typical map interactions include zoom, pan, and object selection.
PAN & ZOOM
Panning allows movement of the map in any direction without change to the current
zoom setting. Zooming adjusts the current magnification level between pre-defined
range parameters.
Before flight, consider which
map scales are best for achieving
the desired level of detail and
map information.
Generally, use smaller map
scales in and around terminal
Maximum Scale
Value
areas and whenever precise
navigation is required (e.g.,
airway or radial intercepts).
During cruise flight, increase the
map scale to better balance
navigation, situational
awareness, and decision
making.
Minimum Scale
Value
OBJECT SELECTION
Tapping any object or location on the map displays a map pointer and an information
banner.
MAP POINTER
This symbol indicates point of contact on the map. A gray circle
highlights any selected waypoint or obstacle.
• Parallel track offsets do not apply to the temporary flight plan
Graphical editing allows quick changes to the active flight plan
from the map display.
Map provides identifier keys for
selecting waypoints that are
stacked or in close proximity. If the
displayed options are not preferred,
tap away or select Cancel.
3. Tap and drag the leg to a
new waypoint or airway,
then release.
The temporary flight plan
adjusts to show the new route.
If no other edits are necessary,
tap Done.
The new waypoint now appears
in the active flight plan.
Delete any existing flight plan before attempting to graphically edit a direct-to
waypoint. Map does not allow the addition of an intermediate waypoint
between the current position and a direct-to waypoint unless the waypoint is in
the flight plan.
ETAEstimated time of arrivalTrip TimerTimer display
ETA at Dest ETA at destinationTRKTrack
ETEEstimated time en routeVSRVertical speed required
ETE to DestETE to destinationWindWind speed and direction
Generic
Timer
GSGPS ground speedOFFDo not display data field
GSLGPS altitude
Distance/bearing from
destination airport (i.e.,
the straight line distance)
Distance to destination
(i.e., the distance along
the flight plan)
Timer displayXTKCross track error
OAT (static)
TimeCurrent time
Time to
TOD
Outside static air
temperature
Outside total air
temperature
Time to top of descent
“Destination” refers to the missed approach point (if an approach is loaded) or
the final airport in the flight plan.
3.2.2Map Orientation
Sets the orientation of the map display.
Options include North Up, Track Up, or Heading Up.
Label below the North indicator shows the current orientation.
This label is absent when the info banner is active.
North Up is useful when zoomed out to view the entire route or a frontal system
on a NEXRAD display.
Sets the range at which map orientation changes to North Up.
Using the North Up Above feature causes the screen to switch at certain zoom
levels. This is useful as a shortcut to quickly increase situational awareness.
3.2.4Visual Approach
Sets the distance from the
destination airport at which the
Visual Approach selector key
becomes active.
Visual Approach
Key
To reduce page clutter, the key moves to the upper
left corner of the display when the info banner is
active.
• Indication absent when aircraft velocity is < 30 kt
Provides a more precise indication
of distance between the aircraft
and map objects.
Indicates the current ground track.
Arrow tip represents aircraft position
at the specified time interval
(if the aircraft maintains current
ground track during that time).
Track vector length options display as a dashed line and arrow extending from
the aircraft icon, showing current track and distance the aircraft will travel in the
selected time.
If the track vector is placed over a point on the map, and no data is entered into
the system, the unit indicates a wind-corrected GPS track to that point. This is
useful for intercepting airways and radials, making small but positive lateral
corrections during approaches, and in setting up for arrivals in the terminal area.
3.2.8Ahead View
FEATURE LIMITATIONS
• Not available when page orientation is North Up
Repositions ownship near the
bottom of the page to expand the
view ahead.
Control keys enable the specified overlay function only and
do not activate interfaced equipment. Control keys remain
active even in the absence of required data.
Overlay controls reside in the Map menu.
TOPO
Overlay data controls reside in the
Map menu. Changes to an overlay
setting take effect immediately.
NEXRAD and Terrain overlays are
mutually exclusive. Enabling one
automatically disables the other.
Icons indicate which overlays are present at the current map range. A crossed out
icon means the overlay is active, but data is unavailable due to a failure, test, or
standby condition (where relevant).
The absence of an overlay icon means one of two possible conditions:
1. Overlay not present at the current detail level or zoom setting.
SafeTaxi hot spots identify locations on an
airport surface where positional confusion
or runway incursions are likely to occur.
These known problem areas require
heightened attention by pilots.
Selecting the border of a hot
spot displays a brief summary of
the indicated hazard and an
information key.
Tapping this key provides additional location information.
Numbering corresponds to a list on the airport diagram.
The following airport features
may be deemed hot spots by
aviation authorities.
• Intersecting taxiways and
runways
• Complex ramp areas
• Directional limitations
• Limited wing-tip clearance
• Overflight risk
CONSTRUCTION SPOTS
There are no expanded detail keys or notes
associated with construction areas.