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 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.
Garmin International, Inc.
1200 E. 151
st
Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482
www.garmin.com
Garmin (Europe) Ltd
Liberty House
Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, UK
Telephone: +44 (0) 8708501241
RECORD OF REVISIONS
Revision
Revision
Date
A 08/26/09 Initial Release
Description
Page A G3X Installation Manual
Revision A 190-01115-01
WARNING
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
The Garmin G3X system includes products like the GDU 37X and the GSU 73 that are
not TSO-certified products and have received no FAA approval or endorsement.
Consequently the G3X system is not suitable for installation in type-certificated aircraft.
NOTE
Unless otherwise noted all installation guidance, requirements, and instructions apply to
one-display, two-display, and three-display G3X systems.
NOTE
References to the GDU 37X throughout this manual apply equally to the GDU 370 and
GDU 375 except where specifically noted.
INFORMATION SUBJECT TO EXPORT CONTROL LAWS
This document may contain information which is subject to the Export Administration
Regulations (“EAR”) issued by the United States Department of Commerce (15 CFR,
Chapter VII Subchapter C) and which may not be exported, released or disclosed to
foreign nationals inside or outside the United States without first obtaining an export
license. The preceding statement is required to be included on any and all reproductions
in whole or in part of this manual.
2.7 Unit Installation................................................................................................................................2-5
4.7 Unit Installation................................................................................................................................4-7
5.5 Unit Installation................................................................................................................................5-4
G3X Installation Manual Page ix
190-01115-01 Revision A
Limited Warranty for Garmin GMU 44 and GTP 59 Products
The Garmin products GMU 44 and GTP 59 are warranted to be free from defects in materials or
workmanship for two years from the date of purchase. Within this period, Garmin will at its sole option,
repair or replace any components that fail in normal use. Such repairs or replacement will be made at no
charge to the customer for parts or labor, provided that the customer shall be responsible for any
transportation cost. This warranty does not cover failures due to abuse, misuse, accident or unauthorized
alteration or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF
ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY
LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU
SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR
CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR
INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to
you.
Garmin retains the exclusive right to repair or replace the unit or software or offer a full refund of the
purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE
REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in
locating a Service Center near you, call Garmin Customer Service at one of the numbers shown below.
Products sold through online auctions are not eligible for rebates or other special offers from Garmin.
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.
Garmin International, Inc. Garmin (Europe) Ltd.
1200 East 151
st
Street Liberty House, Bulls Copse Road
Olathe, Kansas 66062, U.S.A. Hounsdown Business Park
Phone: 913/397.8200 Romsey, SO40 9RB, U.K.
Page x G3X Installation Manual
Revision A 190-01115-01
Limited Warranty for GSU 73 and GDU 37X Products
The Garmin products GSU 73 and GDU 37X are warranted to be free from defects in materials or
workmanship for one year from the date of purchase. Within this period, Garmin will at its sole option,
repair or replace any components that fail in normal use. Such repairs or replacement will be made at no
charge to the customer for parts or labor, provided that the customer shall be responsible for any
transportation cost. This warranty does not cover failures due to abuse, misuse, accident or unauthorized
alteration or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF
ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY
LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU
SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR
CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR
INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply to
you.
Garmin retains the exclusive right to repair or replace the unit or software or offer a full refund of the
purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE
REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in
locating a Service Center near you, call Garmin Customer Service at one of the numbers shown below.
Products sold through online auctions are not eligible for rebates or other special offers from Garmin.
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.
Garmin International, Inc. Garmin (Europe) Ltd.
1200 East 151
st
Street Liberty House, Bulls Copse Road
Olathe, Kansas 66062, U.S.A. Hounsdown Business Park
Phone: 913/397.8200 Romsey, SO40 9RB, U.K.
G3X Installation Manual Page xi
190-01115-01 Revision A
GSU 73 HARDWARE MOD LEVEL HISTORY
The following table identifies hardware modification (Mod) Levels for the GSU 73 LRU. Mod Levels
are listed with the associated service bulletin number, service bulletin date, and the purpose of the
modification. The table is current at the time of publication of this manual (see date on front cover) and is
subject to change without notice.
MOD
LEVEL
SERVICE
BULLETIN
NUMBER
SERVICE
BULLETIN
DATE
PURPOSE OF MODIFICATION
1 N/A N/A Improved HSCM accuracy when using +28V supply
Page xii G3X Installation Manual
Revision A 190-01115-01
1 G3X Installation Overview
1.1 Unpacking Unit
Carefully unpack the equipment and make a visual inspection of the unit for evidence of damage incurred
during shipment. If any component of the G3X system is damaged, notify the carrier and file a claim. To
justify a claim, save the original shipping container and all packing materials. Do not return the unit to
Garmin until the carrier has authorized the claim.
Retain the original shipping containers for storage. If the original containers are not available, a separate
cardboard container should be prepared that is large enough to accommodate sufficient packing material
to prevent movement.
1.2 Introduction
This manual provides all of the mechanical and electrical information required for the installation of the
G3X system.
NOTE
The Garmin G3X system includes products like the GDU 37X and the GSU 73 that are
not TSO-certified products and have received no FAA approval or endorsement.
Consequently the G3X system is not suitable for installation in type-certificated aircraft.
The following outline describes the organization of this manual:
Section 1
This section contains a basic overview of the G3X system and interface. A Block
diagram is given to aid in the understanding of the system. This section also contains
generic information that pertains to all components of the G3X system, such as
mounting, wiring, and antenna location.
Section 2
This section describes the mechanical, electrical, and installation aspects of the
GDU 37X.
Section 3
This section describes the mechanical, electrical, and installation aspects of the
GMU 44.
Section 4
This section describes the mechanical, electrical, and installation aspects of the
GSU 73.
Section 5
This section describes the mechanical, electrical, and installation aspects of the
GTP 59.
Section 6
This section describes the mechanical, electrical, and installation aspects for the GPS
and XM antennas.
Section 7
Section 8
This section describes the non-G3X LRU interfaces.
This section contains software, configuration, database, and XM activation
information.
Section 9
This section contains post-installation checkout and calibration procedures for the
G3X.
Section 10
Section 11
This section contains G3X troubleshooting information. This section contains information for ensuring the unit is suitable to be returned to
service.
Appendix A
Appendix B
Appendix C
Appendix D
Appendix E
This section contains pinout information for all G3X LRU’s.
This section contains connector installation instructions.
This section contains G3X Outline and Installation Drawings.
This section contains the G3X Interconnect Drawings.
This section contains the G3X External Interface Drawings.
1.3 System Overview
The G3X is an advanced technology avionics suite designed to integrate pilot/aircraft interaction into one
central system. The system combines primary flight instrumentation, aircraft systems instrumentation,
and navigational information, all displayed on one, two, or three color screens. The G3X system is
composed of several 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 G3X 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 additional information on LRU functions, see
the applicable section of this manual.
1.3.1 System Architecture
Figure 1-1 illustrates an example block diagram of a G3X installation. The flexibility of system allows
the installer to determine the architecture that best fits each installation.
Config Module
Autopilot
GMU 44
GTP 59
Config Module
RS-232
A429
RS-485
RS-232
GNS
430(W)
SL 30/40
(1, 2)
RS-232
ELT
RS-232
GDU 37X (PFD1)
Pitot
CAN
Static
GSU 73
A429 (GPS)
A429 (NAV)
A429 (AIR DATA)
(1)
RS-232
A429 (GPS)
A429 (NAV)
GNS
430(W)
RS-232
GMA 240
STEREO/MONO AUDIO
GDU 37X (MFD)
RS-232
GTX 330
(1)
Figure 1-1. G3X Interconnect Example
GDU 37X (PFD2)
RS-232
Notes:
(1) Maximum of 2 COM/NAV units installed.
(2) GDU 37X to SL40 is TX only.
Page 1-2 G3X Installation Manual –Installation Overview
Revision A 190-01115-01
1.4 General G3X LRU Specifications
1.4.1 Garmin LRU Part Numbers
Table 1-1. G3X LRU Part Numbers
LRU Unit Only Part Number Assembly Part Number
GDU 370 Americas DB 011-01747-15 010-00667-15
GDU 370 Atlantic DB 011-01747-20 010-00667-20
GDU 370 Pacific DB 011-01747-35 010-00667-35
GDU 375 Americas DB 011-01747-30 010-00667-25
GMU 44 011-00870-10 010-00296-10*
GSU 73 011-01817-00 010-00691-00*
GTP 59 011-00978-00* NA
*Included in G3X LRU Kit (K10-00016-00)
Table 1-2. Contents of GDU 37X Assembly (010-00667-XX)
Item Garmin P/N Quantity
GDU 37X 011-01747-XX 1
GDU 37X Connector Kit 011-01921-00 1
GDU 37X Nutplate
SD Card, Dummy 145-00561-00 1
Important Safety and Product Information 190-00720-50 1
GDU 37X Quick Reference Guide 190-01055-00 1
Jeppesen Free Single Update 190-10003-03 1
115-01054-00 1
1.4.2 Power Specifications
All LRUs are capable of operating at either 14 or 28 VDC. Table 1-3 lists current draw specifications.
Table 1-3. G3X LRU Power Requirements
LRU Supply Voltage Current Draw
GDU 37X 10-29 Vdc
GMU 44 12Vdc (from GSU 73)Inc. in GSU Current Draw
All width, height, and depth measurements are taken with unit rack (if applicable) and connectors.
Table 1-4. G3X LRU Physical Specifications
LRU Width Height
GDU 370
GDU 375
GMU 44
GSU 73
6.04 inches
(153.4 mm)
6.04 inches
(153.4 mm)
N/A
5.50 inches
(139.8 mm)
7.83 inches
(198.8 mm)
7.83 inches
(198.8 mm)
2.10 inches
(5.33 cm)
3.96 inches
(100.6 mm)
Depth
(GMU 44
Diameter,
including
flange*)
3.41 inches
(86.7 mm)
3.41 inches
(86.7 mm)
*3.35 inches
(85.1 mm)
7.33 inches
(186.2 mm)
Unit Weight
1.6 lbs
(0.713 kg)
1.7 lbs
(0.753 kg)
0.35 lbs.
(0.16 kg)
3.1 lbs
(1.41 kg)
Unit Weight
w/Nutplate
& Connector
Weight
1.8 lbs
(0.803 kg)
1.9 lbs
(0.843 kg)
0.50 lbs.
(0.23 kg)
3.5 lbs
(1.59 kg)
1.4.4 Cooling Requirements
While no forced cooling air is required for the G3X system, it is highly recommended that the air behind
the panel be kept moving (by ventilation or a fan).
• No cooling air is required for the GDU 37X
• No cooling air is required for the GMU 44
• No cooling air is required for the GSU 73, however the GSU 73 should be mounted in a location
that provides adequate airflow to comply with the maximum outer case temperature listed in
Section 4.
NOTE
Avoid installing the G3X LRUs near heat sources. If this is not possible, ensure that
additional cooling is provided. Allow adequate space for installation of cables and
connectors. The installer will supply and fabricate all of the cables. All wiring should be
in accordance with FAA AC 43.13-1B and AC 43.13-2A.
Page 1-4 G3X Installation Manual –Installation Overview
Revision A 190-01115-01
1.5 Installation Requirements
One GDU 37X assembly (listed in Table 1-1) is required, dependent upon customer’s desired database
region. Each GDU 37X (010-00667-XX) comes with all equipment needed for installation.
1.5.1 Required Accessories
The following kits are required for the installation of the G3X.
Table 1-5. Contents of G3X Installation Kit (K10-00017-00)
Item Garmin P/N Quantity
GMU 44, Connector Kit 011-00871-00 1
Config Module w/EEPROM, Jackscrew 011-00979-20 1
Config Module w/Sockets, Jackscrew 011-00979-22 1
Thermocouple Kit 011-00981-00 1
GSU 73, Connector Kit, P9731 011-01818-00 1
GSU 73, Connector Kit, P9732 011-01818-01 1
G3X, Supplemental Parts 011-02347-00 1
GMU 44, Install Rack, Modified 115-00481-10 1
Table 1-6. Contents of G3X LRU Kit (K10-00016-00)
Item Garmin P/N Quantity
GMU 44, Unit Only 010-00296-10 1
GSU 73, Unit Only 010-00691-00 1
GTP 59, Unit Only 011-00978-00 1
1.6 Mounting
Refer to Section 2 through Section 6 for specific mounting instructions for each component of the G3X,
and to Appendix A for Outline & Installation Drawings.
1.7 Wiring/Cabling Considerations
Use MIL-W-22759/16 (or other approved wire) AWG #24 or larger wire for all connections unless
otherwise specified. The supplied standard pin contacts are compatible with up to AWG #22 wire. In
cases where some installations have more than one LRU sharing a common circuit breaker, sizing and
wire gauge is based on aircraft circuit breaker layout, length of wiring, current draw on units, and internal
unit protection characteristics. Do not attempt to combine more than one unit on the same circuit breaker.
RG400 or RG142 coaxial cable with 50 Ω nominal impedance and meeting applicable aviation
regulations should be used for the installation.
Allow adequate space for installation of cables and connectors. Ensure that routing of the wiring does not
come in contact with sources of heat, RF or EMI interference. Analog Input wires routed too close to
spark plugs, plug wires, or magnetos may result in erratic readings.
The installer shall supply and fabricate all of the cables. Required connectors, etc. are provided with the
G3X Installation Kit (K10-00017-00). Electrical connections are made through D subminiature
connectors for the GDU 37X and GSU 73 units, and through a round 9-pin connector for the GMU 44.
Appendix A defines the electrical characteristics of all input and output signals. Required connectors and
associated hardware are supplied with the connector kit..
CAUTION
Check wiring connections for errors before connecting any wiring harnesses. Incorrect
wiring could cause internal component damage.
Table 1-7. Pin Contact and Crimp Tools Part Numbers
LRU Contact Type
GDU 37X
GSU 73
GTP 59
011-00979-20
(Config
module
w/EEPROM
kit)
011-00981-00
(thermocouple
kit)
GMU 44
011-00979-22
(Config
module
w/Sockets &
Jackscrew kit)
Socket, Mil
Crimp, Size 20
Pin, Mil Crimp,
Size 22D
Socket, Mil
Crimp, Size 20
Socket, Mil
Crimp, Size 20,
26-30 AWG
1. Insertion/Extraction tools from ITT Cannon are all plastic; others are plastic with metal tip.
2. Non-Garmin part numbers shown are not maintained by Garmin and consequently are subject
to change without notice.
Garmin
Contact Part
Number
336-00094-00
336-00021-00
336-00022-00
336-00022-01
Recommended
Positioner
M22520/2-08,
Daniels K13-1
Positronic P/N
9502-4,
ITT P/N
M22520/2-09,
Daniels P/N K42
M22520/2-08,
Daniels K13-1
Positronic P/N
9502-5
NOTES
Recommended
Insertion/
Extraction Tool
M81969/1-04
for size 22D
pins and
M81969/1-02
for size 20 pins
Recommended
Hand Crimping
Tool
M22520/2-01
Page 1-6 G3X Installation Manual –Installation Overview
Revision A 190-01115-01
1.7.2 Cable Location Considerations
Use cable meeting the applicable aviation regulation for the interconnect wiring. Any cable meeting
specifications is acceptable for the installation. When routing cables, observe the following precautions:
• All cable routing should be kept as short and as direct as possible.
• Check that there is ample space for the cabling and mating connectors.
• Avoid sharp bends in cabling.
• Avoid routing near aircraft control cables.
• Avoid routing cables near power sources (e.g., 400 Hz generators, trim motors, etc.) or near
power for fluorescent lighting.
• Route the GPS antenna cable as far as possible away from all COM transceivers and antenna
cables.
1.7.3 Cable Installation
1. Route the coaxial cable to the unit location. Secure the cable in accordance with good aviation
practices.
2. Trim the coaxial cable to the desired length and install the BNC connector (330-00087-00) per
the cabling instructions on Figure 1-2. If the connector is provided by the installer, follow the
connector manufacturer’s instructions for cable preparation.
Figure 1-2. Coaxial Cable Installation
3. Contacts for the 50, 62, and 78 pin connectors must be crimped onto the individual wires of
the aircraft wiring harness. Table 1-7 lists contact part numbers (for reference) and
recommended crimp tools.
Connector kits include backshell assemblies. The backshell assembly houses the configuration module
and a thermocouple reference junction (if applicable, see Appendix D). Garmin’s backshell connectors
give the installer the ability to quickly and easily terminate shield grounds at the backshell housing. The
instructions needed to install the Jackscrew Backshell, Configuration Module, and Thermocouple are
located in Appendix B.
NOTE
The GDU 37X rear connector (J3701) is electrically isolated. For installations using
shielded cables, a ground pin must be tied to the connector shell.
Page 1-8 G3X Installation Manual –Installation Overview
Revision A 190-01115-01
2 GDU 37X
Figure 2-1. GDU 37X Unit View
2.1 Equipment Description
NOTE
There is no TSO/ETSO applicable to the GDU G37X.
The GDU 37X provides a central display and user interface for the G3X system. The display is mounted
flush to the aircraft instrument panel using four #6 screws. The GDU 37X is available in two models,
GDU 370 and GDU 375. The GDU 370 is a Garmin Display Unit with a VFR WAAS-GPS receiver.
The GDU 375 provides these same features plus an XM receiver.
2.1.1 Navigation Functions
• Display of position and ground speed
• Display of stored navigation and map databases
• Area navigation functions using the determined position/velocity and stored navigation data
• Advisory approach navigation functions and associated databases
The GDU 37X uses a high-sensitivity GPS receiver that continuously tracks and uses up to 12 satellites to
compute and update its position.
Table 2-3. GDU 37X GPS Specifications
Characteristics Specifications
Acquisition Time a) Warm Start (position known to 10 nm, time known to 10
minutes, with valid almanac and ephemeris): Less than 5
seconds
b) Cold Start (position known to 300 nm, time known to 10
minutes, with valid almanac): Less than 45 seconds
c) AutoLocate™ (with almanac, without initial position or
time): Less than 60 seconds
Update Rate 5/second, continuous
Positional Accuracy <10 meters
Antenna Power Supply Voltage (4.5 to 5.0), current (50 mA max)
Table 2-4 lists Garmin and non-Garmin antennas currently supported by the GDU 37X. Refer to Section
6 for Garmin antenna installation information. For non-Garmin antennas, follow the manufacturer’s
installation instructions.
NOTE
Only a single GPS antenna is required for installations using more than
one GDU 37X unit, as the GDU 37X will “share” the GPS information
with all GDU 37X units.
Table 2-4. GDU 37X Supported Antennas
Model Mount Style
Comant
2480-201
VHF/GPS
[1]
Comant
420-10 XM
only
Antenna
Screw
Mount,
Teardrop
Footprint
Screw
Mount,
ARINC 743
Footprint
Conn
Type
BNC
TNC
Antenna
Type
VHF
COM,
GPS
Mfr
Comant CI 2480-201 N/A
Antenna Part
Number
TNC XM Comant CI 420-10 N/A
Garmin Order
Number
Suction Cup,
GA 26C
Magnetic or
BNC GPS Garmin 011-00149-04 010-10052-04
Flange Mt
GA 26XM
Ground
Plane Mt
TNC XM Garmin 013-00268-10 010-11373-00
GA 55 Stud Mount TNC XM Garmin 011-01033-00 010-10600-01
GA 55A ARINC 743 TNC XM Garmin 011-01153-00 010-10598-00
GA 56 Stud Mount BNC GPS Garmin 011-00134-00 010-10040-01
Screw
GA 57X
[2]
Mount,
ARINC 743
BNC
TNC
GPS
XM
Garmin 011-01032-10 010-11370-10
Footprint
[1] The GPS antenna connec tor is TNC type. The VHF COM antenna connector is BNC type.
NOTE
The GPS antenna should provide a gain of 16 to 25dB, and requires a
4.5V to 5V supply voltage that can provide 50mA max.
2.3 Environmental Specifications
The GDU 37X has an Operating Temperature Range of -20°C to +60°C.
The GDU 37X Connector Kit is provided with the GDU 37X unit and is required to install the unit
(Figure 2-2). The GDU 37X Nutplate (115-01054-00) is also supplied with the unit to reinforce the panel
cutout in thin panel installations.
The contents of the GDU 37X Connector Kit are listed in Table 2-5. One kit is required for each GDU
37X installed.
Table 2-5. Contents of GDU 37X Connector Kit (011-01921-00)**
Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are
recommended for installation of the GDU 37X. Refer to Section 1.6 for wiring considerations and to
Appendix A for pinouts.
Connector kits include backshell assemblies. Garmin’s backshell connectors give the installer the ability
to quickly and easily terminate shield grounds and install a configuration module (PFD1 only) at the
backshell housing. The instructions needed to assemble the backshell connector w/Shield Block
grounding system and configuration modules are located in Appendix B.
NOTE
The GDU 37X rear connector (J3701) is electrically isolated. For
installations using shielded cables, a ground pin must be tied to the
connector shell.
2.6 Mounting Requirements
Refer to Appendix C for outline and installation drawings.
2.7 Unit Installation
The GDU 37X is installed by holding the unit flush with the instrument panel and fastening the four
captured 3/32” hex socket head screws to the panel as shown in Figures C-1.1 and C-1.2.
2.8 Maintenance
Maintenance of the GDU 37X is “on condition” only. Periodic maintenance of the GDU 37X is not
required. Instructions for Continued Airworthiness (ICA) are not required for this product under 14 CFR
Part 21 since the GDU 37X has received no FAA approval or endorsement.
The below drawing can be used as a template when marking the panel for cutout. Dimensions below are
to verify accuracy of printout only, see Figure C-1.2 for complete dimensions.
GDU 37X PANEL CUTOUT TEMPLATE
IMPORTANT!
Ensure the Page Scaling setting
is set to NONE when printing
this page. Verify dimensions
of printed template are
accurate before cutting panel.
The Garmin GMU 44 Magnetometer is a remote mounted device that interfaces with a Garmin GSU 73 to
provide flight attitude and heading data for flight instrumentation.
An Attitude and Heading Reference System combines the functions of a Vertical Gyro and a Directional
Gyro to provide measurement of Roll, Pitch and Heading angles. The Garmin ADAHRS and
magnetometer replace traditional rotating mass instruments.
Using long-life solid-state sensing technology, the GMU 44 Magnetometer uses magnetic field
measurements to create an electronically stabilized AHRS.
The GMU 44 magnetometer provides magnetic information to support the function of the GSU 73. The
GSU 73 provides operating voltage to the GMU 44 Magnetometer.
3.1.1 Interface Summary
The following is an interface summary for the GMU 44.
Supply Voltage: 14/28 VDC. See Table 1-3 for current
specifications.
3.3 Environmental Specifications
Table 3-2 lists general environmental specifications.
Table 3-2. GMU 44 Environmental Specifications
Specification Characteristic
Regulatory Compliance RTCA/DO-160D Environmental Conditions and
EUROCAE/ED-14D
Unit Software RTCA/DO-178B Level B
Operating Temperature
Range
-55° C to +70° C
Altitude 55,000 Feet
3.4 GMU 44 TSO/ETSO Compliance
Table 3-3. TSO/ETSO Compliance
Applicable
Custom Logic
Device Part
Numbers
All
006-C0048-0(_)
Function
Direction Instrument,
Magnetic (Gyroscopically
Stabilized)
TSO/ETSO/SAE/
RTCA/EUROCAE
TSO-C6d
ETSO-C6d
AS8013A
Category
Applicable LRU
SW Part
Numbers
All
006-B0224-(__)
except
006-B0224-Z(_)
3.4.1 TSO/ETSO Deviations
The following table provides a list of applicable TSO and SAE deviations for the GMU 44.
Table 3-4. TSO/ETSO Deviations
TSO Deviation
TSO-C6d
(GMU 44)
ETSO-C6d
(GMU 44)
1. Garmin was granted a deviation from TSO-C6d to use RTCA DO-160D instead of RTCA
DO-160B as the standard for Environmental Conditions and Test Procedures for Airborne
Equipment.
2. Garmin was granted a deviation from TSO-C6d to use RTCA DO-178B instead of RTCA
DO-178A to demonstrate compliance for the verification and validation of the computer
software.
3. Garmin was granted a deviation from TSO-C6d to use SAE AS 8013A instead of SAE
AS 8013 as the Minimum Performance Standard.
4. Garmin was granted a deviation from TSO-C6d to list this secondary TSO in the
Installation Manual rather than on the article itself.
5. Garmin was granted a deviation from TSO-C6d to list the DO-178B software level in the
Installation Manual rather than on the article itself.
1. Garmin was granted a deviation from ETSO-C6d to use RTCA DO-160D instead of SAE
AS 8013 as the standard for Environmental Conditions and Test Procedures for Airborne
Equipment.
2. Garmin was granted a deviation from ETSO-C6d to use SAE AS 8013A instead of SAE
AS 8013 as the Minimum Performance Standard.