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ARTEX PRODUCTS / ACR ELECTRONICS, INC.

DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL

DGL-1, DONGLE (453-4010)

570-4010 Rev. G

Company Confidential

Page 16 of 30

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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Summary of Contents for DGL-1

Page 1: ...g Adapter 453 4010 Description Operation Installation and Maintenance Manual 570 4010 Rev G Artex Products ACR Electronics Inc 5757 Ravenswood Road Fort Lauderdale FL 33312 Phone 954 981 3333 Fax 954 983 5087 www acrartex com ...

Page 2: ...mentation 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 Tel...

Page 3: ...0 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 Req...

Page 4: ...licability 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 Informati...

Page 5: ...eacon 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 alterati...

Page 6: ...le 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 Don...

Page 7: ...ial 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 ...

Page 8: ...NICS 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 ...

Page 9: ...utes 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 applica...

Page 10: ...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 Standar...

Page 11: ...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 Reprogr...

Page 12: ...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 Standar...

Page 13: ... 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 2...

Page 14: ...riodic 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 M...

Page 15: ... 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 additio...

Page 16: ...rational 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 wir...

Page 17: ...Confidential Page 17 of 30 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 ...

Page 18: ...ics 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 ...

Page 19: ... 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...

Page 20: ... 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 ...

Page 21: ...ounding considerations and recommendations are applicable a Minimum 22 AWG wire size b Shielding is recommended to help prevent EMI and RF interference c Use high quality conductor meeting MIL W 16878 M22759 M27500 or a commercial equivalent acceptable for use in aircraft applications d Provide a Drip Loop at the Dongle and the ELT receptacle to divert moisture from the connections See Error Refer...

Page 22: ...ness Arrangement 3 A preassembled wire harness P N 611 4010 is provided with the Dongle NOTE Disassembly of the 12 position rectangular connector is required when installing a Dongle on an aircraft previously equipped with an ARTEX ELT to integrate the wire harness Refer to Figure 6 Molex 12 Pin Connector Harness Arrangement on page 22 Use Molex extraction tool Molex P N 11 03 0002 or an equivalen...

Page 23: ...olex Power and Ground Wires on page 23 CAUTION DO NOT WIRE DONGLE DIRECTLY TO THE AIRCRAFT BATTERY THE 28 VOLT DC POWER SOURCE SHOULD BE PROTECTED WITH A 5A FUSE OR CIRCUIT BREAKER AND ON A SWITCH BUS a A Raychem solder sleeve splice Raychem P N D 1744 01 is provided for this connection NOTE Refer to Raychem for specific instructions on the splice use Alternate splices may be used if installed in ...

Page 24: ... the black circular connector to the plug on the Dongle Figure 8 Dongle Wiring Diagram C 24 Bit Address Reprogramming 1 The 24 bit address is composed of binary 1s and 0s with a 1 electrically grounded to the airframe and 0 electrically open 2 Encoding is accomplished by using a 24 bit address switch block which internally grounds selected addresses 3 Remove the Dongle in accordance with Dongle Re...

Page 25: ... Conversion 5 Set the 24 bit address switch block switches as appropriate for the 24 bit address binary code determined in the previous step See Figure 10 24 Bit Address Switch Block on page 25 6 Install the Dongle in accordance with Dongle Installation on page 20 Figure 10 24 Bit Address Switch Block 7 Test the installation in accordance with 24 Bit Address Reprogramming Verification Test on page...

Page 26: ...er to the illustration in the applicable IPL figure to find attaching hardware and related assembly parts 3 In cases where multiple item numbers are shown on an illustration for the same item there is more than one part number option associated with that item 2 Manufacturer Name and Address A Ordering Information 1 Approved parts may be ordered from ACR Electronics Inc or any authorized dealer CON...

Page 27: ...rvice bulletin are annotated to indicate both pre and post service bulletin configurations The term PRE SB XXXX in the Nomenclature column designates the original configuration and the term POST SB XXXX identifies assemblies and parts after the modification has been completed 4 The terms defined below are used when applicable to indicate the interchangeability of parts Term Abbreviation Definition...

Page 28: ...Company Confidential Page 28 of 30 D UPA Units Per Assembly Column 1 The quantity shown in this column represents the units required for one next higher assembly or when referring to attaching parts the quantity to attach one such item 2 The abbreviation RF reference indicates the end item assembly is listed for reference purposes ...

Page 29: ...of 30 4 Detailed Parts List Figure 11 DGL 1 Dongle Programming Adapter Assembly FIG ITEM PART 1234 NOMENCLATURE UPA 11 01 453 4010 Programming Adapter Assembly DGL 1 Dongle 1 02 452 4010 DGL 1 Dongle Main Assembly 1 ATTACHING PARTS 03 402 4011 Cover Dongle DGL 1 1 04 201 6324 01 Screw 6 32x5 16 PHIL TRUSS S S 8 05 452 3052 03 Cover Top Protective w inserts 1 ...

Page 30: ...mpany Confidential Page 30 of 30 Figure 12 Wire Harness FIG ITEM PART 1234 NOMENCLATURE UPA 12 01 611 4010 Harness DGL 1 Dongle 1 ATTACHING PARTS 455 4010 01 Install Kit DGL 1 1 151 6627 Terminal Crimp Male 062 Dia 6 591 0999 Label Hex Code 1 591 0429 01 Label Country and Country Code 1 610 1744 01 Solder sleeve Wire Splice 10 in 2 ...

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