ARTEX DGL-1 Manual
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 2 of 30
PROPRIETARY INFORMATION
This document contains proprietary information and such information may not be disclosed to others for any
purpose, nor used for manufacturing purposes without written permission from ACR Electronics.
Information in this manual is subject to change without notice. ACR Electronics makes no warranty, expressed
or implied, with regard to this manual, including but not limited to any implied warranties of merchantability,
fitness for a particular purpose, and non-infringement. In addition, ACR Electronics makes no warranty with
regard to the documentation or data contained herein. ACR Electronics is not liable in the event of incidentals,
special, consequential, or any other damages in connection with or arising from furnishing, performance, or use
of this manual.
Reproduction of this publication or any portion thereof by any means is prohibited. For further information
contact Sales, ACR Electronics, 5757 Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (954) 981-3333.
AIRWORTHINESS LIMITATIONS
The Airworthiness limitations section is FAA approved and specifies inspections and other maintenance required
under 14 CFR§ 43.16 and 91.403, unless an alternative program has been approved.
IMPORTANT NOTICE
ACR Electronics will be responsible for full distribution and revisions of ICA’s (Instructions for Continued
Airworthiness). For inquiries regarding the content and currency of this manual, contact ACR Electronics, 5757
Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (954) 981-3333.
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 3 of 30
TABLE OF CONTENTS
TABLE OF CONTENTS ...............................................................................................................................3
LIST OF ACRONYMS, ABBREVIATIONS AND DEFINITIONS ..........................................................................5
LIST OF FIGURES .....................................................................................................................................6
RECORD OF REVISIONS ............................................................................................................................7
SERVICE BULLETIN LIST ...........................................................................................................................8
INTRODUCTION .......................................................................................................................................9
1. Manual Usage ................................................................................................................................9
A. General .................................................................................................................................9
B. Application ............................................................................................................................9
2. Model Descriptions .......................................................................................................................10
A. Dongle DGL-1 Programming Adapter..................................................................................... 10
3. Approvals ....................................................................................................................................10
A. Dongle DGL-1 ...................................................................................................................... 10
4. References ..................................................................................................................................10
A. Regulatory Documents ......................................................................................................... 10
B. Other Documents.................................................................................................................10
DESCRIPTION AND OPERATION .............................................................................................................. 11
1. Description ..................................................................................................................................11
A. Functional Overview ............................................................................................................. 11
B. Components ........................................................................................................................11
C. 24-Bit Address Reprogramming Functionality .........................................................................11
2. Operation ....................................................................................................................................12
A. Operational Overview ...........................................................................................................12
3. Specifications...............................................................................................................................13
A. Electrical ............................................................................................................................. 13
B. Physical............................................................................................................................... 13
TEST AND FAULT ISOLATION .................................................................................................................. 14
1. General .......................................................................................................................................14
A. Applicability ......................................................................................................................... 14
B. Regulatory Requirements ..................................................................................................... 14
2. Inspection ...................................................................................................................................14
A. Periodic Inspection...............................................................................................................14
3. Test Procedures ...........................................................................................................................14
A. General ...............................................................................................................................14
B. 24-Bit Address Reprogramming Verification Test ....................................................................14
C. 15-Digit Hex ID Verification .................................................................................................. 15
4. Fault Isolation..............................................................................................................................16
A. Troubleshooting Guidelines................................................................................................... 16
REMOVAL ............................................................................................................................................... 17
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 4 of 30
1. DGL-1 Programming Adapter ........................................................................................................17
A. Dongle Removal...................................................................................................................17
2. Material or Equipment Return .......................................................................................................18
A. Shipment Information .......................................................................................................... 18
B. Return Material Authorization................................................................................................18
INSTALLATION ....................................................................................................................................... 19
1. Regulatory Requirements and Guidelines .......................................................................................19
A. Applicability ......................................................................................................................... 19
B. TSO C126, Paragraph D .......................................................................................................19
C. FAA..................................................................................................................................... 19
D. Canada................................................................................................................................19
E. Other Countries ................................................................................................................... 19
F. RTCA...................................................................................................................................20
2. Mechanical ..................................................................................................................................20
A. Dongle Location ................................................................................................................... 20
B. Dongle Installation ............................................................................................................... 20
3. Wiring .........................................................................................................................................21
A. General Considerations and Recommendations ......................................................................21
B. Dongle Wiring......................................................................................................................22
C. 24-Bit Address Reprogramming............................................................................................. 24
ILLUSTRATED PARTS LIST ...................................................................................................................... 26
1. Introduction.................................................................................................................................26
A. Purpose............................................................................................................................... 26
B. IPL Usage Guide .................................................................................................................. 26
2. Manufacturer Name and Address ..................................................................................................26
A. Ordering Information ........................................................................................................... 26
3. Explanation of Detailed Parts List Entries .......................................................................................26
A. Fig # & Item Column ........................................................................................................... 26
B. Part # Column .....................................................................................................................26
C. Nomenclature Column .......................................................................................................... 26
D. UPA (Units Per Assembly) Column......................................................................................... 28
4. Detailed Parts List ........................................................................................................................29
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 5 of 30
LIST OF ACRONYMS, ABBREVIATIONS AND DEFINITIONS
Term Definition
AC Advisory Circular –A Federal Aviation Administration (USA) bulletin with special
information. For the purposes of this document, the acronym AC does not refer
to electrical alternating current.
CFR Code of Federal Regulations –The general and permanent rules published in
the Federal Register by the executive departments and agencies of the Federal
Government. Title 14, “Aeronautics and Space” contains the FARs.
COSPAS-SARSAT The international search and rescue consortium that governs the international
satellite-based search and rescue distress alert detection and information
distribution system. For a complete description go to the official web site for
the International COSPAS-SARSAT Program.
Dip Switch A set of manual electric switches packaged in a group in a standard dual in-line
package (DIP).
Drip Loop Extra wire length used to form a U-shaped bend in a wire or cable. Water or
other fluids will flow down to the bottom of the loop and drip off. Electrical
connections are made at the top of the loop.
ELT Emergency Locator Transmitter –ELTs are installed on aircraft and used to
send emergency signals to the SAR satellite system. The word “Beacon” is
associated with these devices.
FAA Federal Aviation Administration –The United States government agency for
aircraft safety and regulation.
FAR Federal Aviation Regulations –The rules and regulations governing the
manufacture, certification, operation, maintenance, repair, and alteration of
aircraft in the United States.
Form 337 FAA Form 337 is required anytime a major repair and/or major alteration is
performed on an aircraft. Refer to FAR, Part 43, Appendix A and the definitions
of Major Repair/Alteration contained in FAR, Part 1 for guidance.
ID Identification
MIL The three-letter acronym that stands for “Military” and proceeds military
specifications and standards numbers (e.g., MIL-W-XXXX would indicate a wire
specification and MIL-STD-XXXX would indicate a standard).
MSB Most Significant Bit - The bit position in a binary number having the greatest
value.
P/N Part Number –Refers to an ACR part number, unless otherwise noted. Part
numbers are also indicated with parentheses (e.g., XXX-XXXX).
Plug The term “Plug”, within the context of this document, refers to the male half of
an electrical connector.
Receptacle The term “Receptacle,” within the context of this document, refers to the
female half of an electrical connector.
RTV A rubbery silicon-based adhesive typically used to prevent vibration problems
and water intrusion.
SAR Search and Rescue
TSO Technical Standard Order –A TSO is a minimum performance standard issued
by the FAA for specified materials, parts, processes, and appliances used on
civil aircraft.
VHF Very High Frequency –The 30 MHz to 300 MHz radio frequency band
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 6 of 30
LIST OF FIGURES
Figure 1 DGL-1 (Dongle) Programming Adapter with ELT Cover ..........................................................10
Figure 2 DGL-1 (Dongle) Programming Adapter Assembly ..................................................................11
Figure 3 Dongle Removal Sequence ..................................................................................................17
Figure 4 Dongle Outline and Dimensions ...........................................................................................20
Figure 5 Dongle Wiring Harness Arrangement.................................................................................... 22
Figure 6 Molex 12-Pin Connector Harness Arrangement......................................................................22
Figure 7 Molex Power and Ground Wires ...........................................................................................23
Figure 8 Dongle Wiring Diagram ....................................................................................................... 24
Figure 9 Octal/Hexadecimal to Binary Conversion...............................................................................25
Figure 10 24-Bit Address Switch Block ............................................................................................... 25
Figure 11 DGL-1 (Dongle) Programming Adapter Assembly ................................................................29
Figure 12 Wire Harness ....................................................................................................................30
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 7 of 30
RECORD OF REVISIONS
REVISION
CHANGE
DATE
REVISION
CHANGE
DATE
-
RELEASE
Nov 06/2002
-
DCN 2124
Dec 18/2002
-
DCN 2147
Feb 17/2003
-
DCN 2188
Apr 21/2003
-
DCN 2369
Apr 21/2004
A
DCN 3144
Dec 11/2007
B
DCA W9612
Apr 06/2010
C
ECO 14756
Jul 28/2011
D
ECO 15119
Jun 27/2012
E
ECO 15487
Sept 23/2013
F
ECO 15897
Feb 20/2015
G
ECO 16761
Oct 9/2017
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 8 of 30
SERVICE BULLETIN LIST
SERVICE
BULLETIN NO
ISSUE
DATE
SUBJECT
MANUAL
REV NO
MANUAL
REV DATE
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 9 of 30
INTRODUCTION
1. Manual Usage
A. General
1) This manual describes the operation, installation, and maintenance of the DGL-1 (Dongle) Programming
Adapter. This information is provided to ensure initial and continued airworthiness. Information
presented in this manual is accurate at time of printing, but is subject to change. Refer to the Artex
products web site at www.acrartex.com for the latest information and any updates to this manual.
2) Web links provided in this manual were accurate at time of printing, but may be subject to change.
3) Regulatory references contained herein are generally confined to United States and Canadian
requirements and, in any case, should not be considered all encompassing. Consult your national
aviation authority for applicable requirements.
B. Application
1) This manual constitutes supporting data/documentation for the Dongle, including:
a) Description and Operation
b) Test and Fault Isolation (includes inspection criteria)
c) Removal
d) Installation
e) Registration
f) Illustrated Parts List
2) In the United States, a 406 MHz ELT must be installed and maintained in accordance with the
requirements herein and 14 CFR, FAR Parts 43, and 91; and other airworthiness requirements, as
applicable.
3) 406 MHz ELT installation and maintenance in all other countries must comply with the requirements
herein and applicable national airworthiness requirements.
4) The accessories (i.e., remote switch) addressed in this manual are the accessories most commonly
associated with a 406 MHz ELT. Other options, such as a different remote switch configuration or a
navigation interface, should be installed and maintained in accordance with the written instructions
specific to the accessory.
NOTE: Contact ACR Electronics, Inc., for optional accessories approved for use with a ME406
Series ELT.
5) To ensure proper operation, only parts listed in the Illustrated Parts List of this manual or those
recommended by ACR Electronics, Inc., may be used as replacement parts for the Dongle.
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 10 of 30
2. Model Descriptions
A. Dongle DGL-1 Programming Adapter
1) The Dongle is a 24-bit address programming adapter with two rows of DIP switches.
2) The Dongle is an optional auxiliary device attached to an ELT top cover that remains with an aircraft to
allow fleet operators to transfer ELTs between aircraft.
Figure 1 DGL-1 (Dongle) Programming Adapter with ELT Cover
3. Approvals
A. Dongle DGL-1
1) FAA TSO-C126 - System Component
2) ETSO 2C126 - System Component
4. References
A. Regulatory Documents
1) The following regulatory documents are referred to herein. When referring to such documents, it is the
manual user’s responsibility to ensure they are using the latest revision or release of such documents. To
that end, the revision designator of specific document numbers has not been included, with the
exception of the RTCA document listing, which reflects the revision level of the documents at the time
of TSO testing and certification.
2) Except in the case of a printed manual, reference documents available on-line or source locations are
linked to applicable web sites.
3) United States
a) AC 43-210, “Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and
Repairs”
b) AC 43.9-1, “Instructions for Completion of FAA Form 337”
c) AC 43-13-1, “Acceptable Methods, Techniques, and Practices –Aircraft Inspection and Repair”
d) AC 43.13-2, “Acceptable Methods, Techniques, and Practices - Aircraft Alterations”
4) COSPAS-SARSAT
a) C/S G.005, “Cospas-Sarsat Guidelines on 406 MHz Beacon Coding, Registration and Type Approval”
b) C/S S.007, “Handbook of Beacon Regulations”
B. Other Documents
1) The following documents are available on-line at the Artex products web site at www.acrartex.com, or
from ACR Electronics upon request.
A) 570-1000, “ELT Test Set (ETS) Operation Manual”
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 11 of 30
DESCRIPTION AND OPERATION
1. Description
A. Functional Overview
1) The Dongle is connected to an ELT to allow the operator to easily program aircraft 24-bit address
(Standard Location Protocol) into a compatible ELT.
2) When power is applied, the Dongle verifies the 24-bit address set locally on its DIP switches matches the
24-bit address stored in the memory of the ELT when power is applied. If the Dongle address matches
the ELT address, the Dongle will shut down. If the ELT address does not match, the Dongle will
program the ELT with its locally set address, and then shut down.
B. Components
1) The Dongle is designed to mount to a protective top cover on the ELT with four screws. See Figure 2
DGL-1 (Dongle) Programming Adapter Assembly.
Figure 2 DGL-1 (Dongle) Programming Adapter Assembly
2) The Dongle can be mounted directly to the airframe within the proximity of the ELT to utilize the
prefabricated cable assembly (P/N 611-4010).
C. 24-Bit Address Reprogramming Functionality
CAUTION: THE PROGRAMMING AND LABELING OF THE ELT MUST MATCH THE
AIRCRAFT IN WHICH IT IS INSTALLED. RE-MARK THE ELT PRODUCT LABEL
AS NECESSARY TO REFLECT NEW PROGRAMMING AND/OR COUNTRY OR
REGISTRY. CONTACT THE LOCAL REGULATORY AUTHORITIES
RESPONSIBLE FOR ELT REGISTRATION AND REFER TO THE APPLICABLE
ELT DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE
MANUAL FOR ELT REGISTRATION REQUIREMENTS.
1) The Dongle provides the means to reprogram ELTs with 24-bit address location protocol programming.
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
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570-4010 Rev. G Company Confidential Page 12 of 30
2) This capability facilitates swapping ELTs from one aircraft to another when performing routine
maintenance, etc., without losing a significant amount of time reprogramming ELTs.
3) If the ELT is not programmed with a 24-bit address location protocol, the Dongle will not reprogram the
ELT.
2. Operation
A. Operational Overview
1) Operation of the Dongle is automatic and requires no operator interface other than activating the +28
VDC power source and verifying no failure mode is present. See Fault Isolation on page 16.
2) The following conditions must be true for the Dongle to function:
a) +28 VDC aircraft power must be applied to the unit (i.e., the power source must be switched on).
b) The Artex ELT must be programmed with a 24-bit address long message (Standard Location
Protocol).
NOTE: The Dongle is designed for use only with Artex ELTs. No other use of the Dongle is
certified or approved by ACR Electronics.
c) The ELT software version must be at least V133M, V134B, or V135C (displayed on the ELT product
label).
3) Once the Dongle verifies or updates the ELT address, it shuts down.
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570-4010 Rev. G Company Confidential Page 13 of 30
3. Specifications
A. Electrical
1) Table 1 lists the electrical specifications of the Dongle.
CRITERIA
PARAMETER
CHARACTERISTIC
Pin 1
RX Input
TTL
Pin 2
TX Output
TTL
Pin 3
5.6 VDC Output
5.6 VDC ±0.3 VDC
Pin 4
Power Input
+28 VDC ±10 VDC
Pin 5
ELT Ground
ELT Pin 11
Pin 6
DGL-1 Ground
Aircraft Ground
Artex ELT Software Compatibility
V133M, V134B, V135C
Table 1 Electrical Specifications
B. Physical
1) Table 2 lists the physical specifications of the Dongle.
CRITERIA
PARAMETER
CHARACTERISTIC
Weight
DGL-1
4.8 ox (90 g)
Protective Top Cover
6.7 oz. (190 g)
DGL-1 Harness
1 oz. (28 g)
Dimensions (L x H x W)
Dongle mounted on ELT Top Cover
10.95 x 2.42 x 3.36 in.
(278 x 61 x 85 mm)
Table 2 Physical Specifications
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TEST AND FAULT ISOLATION
1. General
A. Applicability
1) This section only covers inspection, testing, and fault isolation procedures specific to the Dongle.
2) Refer to the applicable ELT Description, Operation, Installation & Maintenance Manual associated with
the ELT to coordinate the requirements herein with the requirements for inspection, test, and fault
isolation of the ELT system as a whole.
B. Regulatory Requirements
1) The Dongle is considered an integral part to the ELT system, and as such is subject to the periodic
inspection and testing required by the regulatory authorities governing the installation, operation, and
maintenance of ELT systems.
2) Refer to the applicable ELT Description, Operation, Installation & Maintenance Manual associated with
the ELT for references to the regulatory requirements.
3) Inspection and testing of the Dongle must be accomplished in conjunction with and on the same
schedule as the ELT and other system components.
2. Inspection
A. Periodic Inspection
1) Remove the Dongle in accordance with Removal on page 17.
2) Perform a visual inspection of the physical integrity of the case, gasket, and DIP switches, checking for:
a) Damage to the finish,
b) Corrosion,
c) Excessive wear of the mounting holes, and
d) Cracks in the mounting flanges.
3. Test Procedures
A. General
CAUTION: ANY ELT RUNNING V133 SOFTWARE (SEE PRODUCT LABEL) TRANSMITS A
FIXED TEST MESSAGE AT ELT RESET, NECESSITATING A “LIVE”
BROADCAST TO READ THE ACTUAL MESSAGE. ANY ELT RUNNING V134 OR
V135 SOFTWARE TRANSMITS THE ACTUAL 406 MHZ MESSAGE AT RESET.
ALL MUST BE TESTED IN AN RF CONTAINER, SCREEN ROOM, OR
CONNECTED TO A DUMMY LOAD VIA THE ANTENNA COAX CONNECTION.
1) This task consists of two subtask testing requirements:
a) 24-bit address programming test, which verifies ELT/Dongle 24-bit address reprogramming
functionality by initiating reprogramming and checking for the address change or an error
indication.
b) 15-digit hex ID determination, which reads the programmed hex ID, country, and country code
broadcast in the 406 MHz message and provides instructions for relabeling and re-registering the
ELT, as applicable.
B. 24-Bit Address Reprogramming Verification Test
1) This is a recommended periodic test.
NOTE: This test procedure verifies the ELT/Dongle has updated the aircraft 24-bit address ID in the
ELT programming.
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2) The following test procedure incorporates the steps necessary to confirm operation of the Dongle into
the “Installed Transmitter Test” procedure defined in the applicable ELT Description, Operation,
Installation & Maintenance Manual.
3) Remove the Dongle in accordance with Removal on page 17.
4) Change the position of the most significant bit (MSB) DIP switch. Refer to Figure 10 24-Bit Address
Switch Block on page 25.
5) Reconnect the Dongle in accordance with Installation on page 19.
6) Apply power to the ELT/Dongle, while the ELT remains off (i.e. inactive). Reprogramming takes place
within 30 seconds of power up.
7) Monitor the ELT for the next 2 minutes. Refer to the troubleshooting guidelines of the applicable ELT
Description, Operation, Installation & Maintenance Manual.
a) The LEDs on the ELT and remote switch will begin to flash rapidly if reprogramming was NOT
successful.
b) If the LEDs remain off after two minutes, the ELT has been reprogrammed.
8) Verify the 24-bit address has changed as a result of changing the position of the MSB DIP switch.
9) Repeat Steps 3 through 8 to return and verify the original configuration of the Dongle.
C. 15-Digit Hex ID Verification
1) 15-digit hex ID verification should be performed any time a Dongle is installed in an aircraft to verify the
ELT is properly labeled and registered.
2) Perform the following procedure within the first 5 minutes after the hour (UTC), as required by AC
43.13-1, Chapter 12, § 12-22, Note 3.
a) Notify any nearby control tower of your intentions.
b) Verify the ELT/Dongle is powered up and has at least 30 seconds to initialize.
c) Set the 453-1000 ELT Test Set (ETS) beacon reader to receive and decode the ELT digital message.
Refer to the ETS operating manual (570-1000) for ETS operating instructions and additional details.
NOTE: A beacon reader equivalent to the ETS may be used, provided it is capable of receiving
and decoding the 406 MHz digital message.
d) Place the ETS within 30 feet of the aircraft 406 MHz antenna.
e) Activate the ELT by placing the control switch or remote switch in the “ON” position.
f) Allow the ELT to transmit for approximately 5 seconds.
g) Deactivate the ELT and read the test message broadcast at “turn-off”.
NOTE: The ELT LED will flash 5 times to indicate a navigation data failure if an Artex Nav
Interface Unit is not installed with the ELT. The Dongle does not support the position
data function of the ELT. If the ELT flashes other failure codes, refer to the applicable
ELT manual to troubleshoot the problem.
3) The 15 digit hex ID (i.e., Beacon ID) displayed by the ETS is compared to the hex ID on the ELT. If
identical, no further action is necessary. If different:
a) Enter the new hex ID on label P/N 591-0999 and affix it to the ELT over the existing hex ID on the
product label.
b) If country and country code have changed, enter the new information on label (P/N 591-0429-01)
and affix it to the ELT over the existing information on the product label.
c) Re-register the ELT. Refer to the applicable ELT Description, Operation, Installation & Maintenance
Manual for specific ELT registration information and instructions.
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4. Fault Isolation
A. Troubleshooting Guidelines
1) Table 3 provides the Dongle troubleshooting guidelines for installation and operational issues.
SYMPTOM
PROBABLE CAUSE
POSSIBLE SOLUTION
ELT and Remote Switch
flash continuously
Dongle is unable to synchronize
with the ELT
Check the ELT protocol is programmed
with a 24-bit address protocol
Open or short in wiring
Check continuity between pin 1 of circular
connector and pin 12
Check continuity between pin 2 of circular
connector and pin 9 of the rectangular
connector
Check wiring and connections continuity
and security for short other pins
Table 3 Troubleshooting Guide
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REMOVAL
1. DGL-1 Programming Adapter
A. Dongle Removal
1) See Figure 3 Dongle Removal Sequence.
Figure 3 Dongle Removal Sequence
2) Remove black circular connector from the Dongle.
3) Remove the screws attaching the mounting plate to the top cover assembly.
4) Remove the screws attaching the Dongle to the mounting plate.
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2. Material or Equipment Return
A. Shipment Information
1) If any material or equipment is to be returned to the factory, under warranty or otherwise, ACR
Electronics must be notified prior to shipment with the following information:
a) Model and serial number of equipment being returned,
b) Date purchased,
c) Date placed in service,
d) Number of hours in service,
e) Nature and cause of failure, and
f) Remarks, if any.
B. Return Material Authorization
2) Upon receipt of such notice, ACR Electronics, Inc. will issue a Return Material Authorization (RMA)
number which then authorizes return of the material or equipment to the following address:
Repair and Overhaul
Artex Products / ACR Electronics, Inc.
5757 Ravenswood Road
Fort Lauderdale, FL 33312 USA
Phone: (954) 981-3333
Fax: (954) 983-5087
a) Failure to obtain a RMA number and provide the details listed in Error! Reference source not
found. on page Error! Bookmark not defined. may cause unnecessary delay and/or rejection of
the returned material or equipment.
b) All material or equipment returned to the factory must be freight prepaid.
c) Acceptable methods of shipment for international return are Airborne, Burlington Air, DHL, Emery,
Federal Express, UPS International, and World Wide only.
NOTE: Do not use “International Commercial Airlines”, such carriers may cause a loss of
returned material or equipment.
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INSTALLATION
1. Regulatory Requirements and Guidelines
A. Applicability
1) The regulatory requirements and guidelines for ELT installations discussed in the following subtasks are
applicable to installation of the DGL-1 Dongle Programming Adapter and must be applied to the DGL-1
Dongle Programming Adapter. Where the word “ELT” is used in the following subtasks, read “DGL-1
Dongle Programming Adapter”.
B. TSO C126, Paragraph D
1) TSO approval of the ELT does not constitute installation approval. All installations are subject to field
approval for a given airframe by either an approved FAA DER or FAA FSDO. For installations outside the
US, contact your local civil aviation regulatory agency for details.
C. FAA
1) This manual constitutes supporting data, as described in AC43.9-1, Paragraph 6.h.(2) and AC 43-210,
Chapter 2, Paragraph 201(a)(6), and as such may be used as support for FAA field approval of the
ELT/NAV Interface installation.
2) In addition to the procedures outlined herein and in accordance with FAR Part 43, the installer must
adhere to the aircraft manufacturer’s instructions and recommendations and the guidelines provided by
FAA Advisory Circular AC 43.13-2 “Acceptable Methods, Techniques, and Practices - Aircraft
Alterations”, specifically Chapters 1 through 3, 11, and 13.
3) By signing the aircraft logbook, and FAA Form 337, the installer is stating the installation has been
performed in accordance with current FAR requirements and the procedures outlined herein. The
completed Form 337 is provided to the FAA and also becomes a permanent part of the aircraft
maintenance records in accordance with AC43-9, Paragraph 17.
D. Canada
1) All installations must be performed in accordance with Canadian Aviation Regulations (CAR) Part V,
Subparts 37, 51, and 71.
E. Other Countries
1) Installations in aircraft outside of the United States and Canada must be performed in accordance with
applicable regulatory authority rules and regulations.
ARTEX PRODUCTS / ACR ELECTRONICS, INC.
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DGL-1, DONGLE (453-4010)
570-4010 Rev. G Company Confidential Page 20 of 30
F. RTCA
1) DO-204, § 3.1.8 guidelines for mounting a ELT:
a) The ELT shall be mounted to primary aircraft load carrying structures, such as trusses, bulkheads,
longerons, spars, or floor beams.
b) The mounts shall have a maximum static local deflection no greater than 0.1 inches (2.5 mm) when
a force of 100 lbs (450 newtons) is applied to the mount in the most flexible direction. Deflection
measurements shall be made with reference to another part of the aircraft not less than 1 foot (0.3
meters) nor more than 3 feet (1.0 meters) from the mounting location.
2) DO-182, § 6.2.2.b recommends that:
a) To maximize the probability of the ELT transmitting a detectable signal after a crash, all ELT system
components, which must survive a crash intact, e.g., transmitter and external antenna, should be
attached to the airframe in such a manner that the attachment system can support a 100 g load,
(ELT weight x 100, ELT antenna weight x 100, etc.) applied through the center of gravity of the
component (ELT, antenna, etc.) in the plus and minus directions of the three principal axes of the
aircraft.
b) Post-crash critical components of the ELT system, e.g., transmitter and external antenna, should be
mounted as close to each other as possible.
2. Mechanical
A. Dongle Location
CAUTION: AVOID INSTALLING THE DONGLE WHERE IT MAY BE SUBJECTED TO
UNPROTECTED EXPOSURE TO HARSH CHEMICAL FLUIDS, SUCH AS
DEICING COMPOUNDS. THESE TYPES OF CHEMICALS MAY CAUSE DAMAGE
TO FASTENERS AND ELECTRICAL COMPONENTS, AS WELL AS ELECTRICAL
CONNECTOR CORROSION.
1) Mount the Dongle within 2 feet (610 mm) of the ELT, such that the interface harness does not exceed
3 feet (914 mm) including strain relief.
2) The Dongle chassis and ELT are mounted to the same support structure in most installations.
B. Dongle Installation
1) Coordinate the Dongle installation with the ELT installation whenever possible. If the Dongle is an
add-on to an existing ELT installation, extend/modify the existing ELT support structure to
accommodate the Dongle.
2) See Figure 4 Dongle Outline and Dimensions.
Figure 4 Dongle Outline and Dimensions
3) Mount the Dongle on the protective top cover on the ELT with four screws (P/N 201-6324-01)
4) Test the ELT installation in accordance with Test and Fault Isolation on page 14.
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