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INSTALLATION AND OPERATION MANUA - Pin's …

INSTALLATION ANDOPERATION MANUALD ocument Number: 570-4010 Revision -24 Bit Address ProgrammingDongleModel: DGL-1 Artex Aircraft Supplies, Keil Road NEAurora, Oregon 97002 USATel (503) 678-7929, Fax (503) 678-7930E-mail of Contents4 System Requirements6 Installation12 Aircraft Address14 Operation15 Test16 INSTALLATION Finalization18 Scheduled Maintenance19 Trouble Shooting20 Appendix A3 DGL-1 Manual570-4010 System RequirementsEmergency Locator TransmitterArtex ELT with software version V133M, V134B or V135C. TheELT software version is displayed on the ELT product Artex ELT must be programmed with a 24 Bit Address LongMessage Protocol. In general, an ELT programmed with 24 BitAddress Long Message Protocol will have a 999 extension on thepart number.

INSTALLATION AND OPERATION MANUAL Document Number: 570-4010 Revision - 24 Bit Address Programming Dongle Model: DGL …

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Transcription of INSTALLATION AND OPERATION MANUA - Pin's …

1 INSTALLATION ANDOPERATION MANUALD ocument Number: 570-4010 Revision -24 Bit Address ProgrammingDongleModel: DGL-1 Artex Aircraft Supplies, Keil Road NEAurora, Oregon 97002 USATel (503) 678-7929, Fax (503) 678-7930E-mail of Contents4 System Requirements6 Installation12 Aircraft Address14 Operation15 Test16 INSTALLATION Finalization18 Scheduled Maintenance19 Trouble Shooting20 Appendix A3 DGL-1 Manual570-4010 System RequirementsEmergency Locator TransmitterArtex ELT with software version V133M, V134B or V135C. TheELT software version is displayed on the ELT product Artex ELT must be programmed with a 24 Bit Address LongMessage Protocol. In general, an ELT programmed with 24 BitAddress Long Message Protocol will have a 999 extension on thepart number.

2 Example: 453-0000 (999). The 999 extension isapplied at factory to indicate the 24 Bit Address Protocol. Subsequent field programming may have changed the protocol. To verify the protocol type, use the Sarsat Beacon Test Set, ARGM odel 5410 or volt DC power source capable of providing 25mATest Equipment406 Mhz uplink receiver. Artex recommends the Sarsat BeaconTest Set, Model ARG 5410, which is available for rent, or purchase from communication radio tuned to :Standard phillips #2 screw driverRTV 162 or equivalent silicone sealantCrimp Tool, Molex 11-01-0008 or equivalent4 DGL-1 Manual570-4010 Extraction Tool, Molex 11-03-0002 or equivalentHeat gun for Raychem wire spliceRegulatory RequirementsBecause of the critical nature of an ELT and dongle, it is importantthat the INSTALLATION be performed according to the followinginstructions.

3 INSTALLATION of the ELT and dongle requiresexperience with avionics and only licensed technicians shouldinstall this addition to the procedures outlined in this manual, the installermust adhere to the guidelines established in FAA-Advisory Circular , Chapters 1 through 3, 11 and 13 (Acceptable Methods,Techniques and Practices Aircraft Alterations).By signing either the aircraft logbooks or the FAA Form 337, youare stating that the INSTALLATION has been performed in accordancewith the current FARs and with the steps and procedures outlinedin this Manual570-4010 InstallationMechanicalThe dongle has been designed to mount to the protective top cover of the of the ELT with four 6-32 phillips head screws (Part Number201-6324-01).

4 If desired the dongle may be mounted directly tothe airframe, but it must be located within a proximity of the ELTsuch that it can utilize the prefabricated cable assembly (PartNumber 611-4010).ElectricalThe dongle is provided with a preassembled wiring harness (PartNumber 611-4010). On one end of the harness is a black circularconnector. This connector attaches to the dongle and requires noadditional assembly. On the other end of the wiring harness is a12 position rectangular connector. This connector attaches to theELT. This connector is where the dongle, remote switch and hornconnect to the ELT. All of the dongle connections have beenpreassembled, but the remote switch and horn will need to be6 DGL-1 Manual570-4010wired to this connector.

5 Also at this end of the wire harness thereare two loose wires that provide power and ground. Dongle WiringPush the black circular connector through the rectangular hole inthe ELT end cap as shown above. Push the circular plug onto thedongle circular receptacle. The circular plug is a push pullconnector. To remove the connector simply pull the collar on theend of the Manual570-4010 Remote Switch/Horn WiringIf the dongle is being installed on an aircraft that has beenpreviously equipped with an Artex ELT, the 12 position rectangularconnector on the aircraft will need to be disassembled using aMolex extraction tool (Molex part number 11-03-0002) orequivalent.

6 The wiring harness will be reassembled using thedongle wire harness (Part Number 611-4010).1 to Remote Switch, Pin 8 (LIGHT)2 to Horn Power3 to Remote Switch, Pin 5 (RST1)4 to Horn Ground5 to ELT, Pin 8 (Pre-Wired)6 to Remote Switch, Pin 2 (RST2)7 to Remote Switch, Pin 7 (EXT ON)8 to ELT, Pin 5 (Pre-Wired)9 to Dongle, Pin 2 (Pre-Wired)10 to Dongle, Pin 3 (Pre-Wired)11 to Dongle, Pin 5 (Pre-Wired)12 to Dongle, Pin 1 (Pre-Wired)(NOTE: Remote Switch Pin numbers referenced above are for anArtex standard remote switch, part number 345-6197.)8 DGL-1 Manual570-4010 Pin 11 is the grounding point for the ELT. The ELT INSTALLATION and OPERATION manual indicates that pin 11 is connected to aircraftground.

7 When using the dongle pin 11 is preassembled in theprovided wire harness, and the ELT ground will be providedthrough the dongle. The system grounding is further defined in the Ground Wiring section of this wires coming from the horn and the remote switch will need tobe terminated with the male terminal pins provided (Part Number151-6627). Strip about .150 in. of insulation, and tin the ends of the wires. Use a Molex crimp tool (Molex Tool # 11-01-0008) orequivalent to install the provided terminal pins. Insert theterminated wires into their applicable location in the rectangular 12position to the applicable ELT INSTALLATION and OPERATION manual foraddition wiring Volt WiringThe dongle requires a 28 volt DC power source capable ofsupplying 25mA.

8 The power source should be protected with a .5A fuse, or circuit breaker, and on a switched bus. Do not wire thedongle directly to the aircraft the preassembled wire harness (Part Number 611-4010) thereare two unterminated wires. Connect the 28 volt power source to9 DGL-1 Manual570-4010the red wire. A Raychem solder sleeve splice (Raychem #D-1744-01) is provided for this connection. Contact Raychem forspecific instructions on the use of this splice. Alternate splicesmay be used if installed in accordance with FAA AC ,Section 445, Splices in Electrical WiringINSTALLING ELT AND DONGLE. For new ELT and dongleinstallations splice the unterminated black wire on thepreassembled wire harness to an aircraft ground point near theELT.

9 A Raychem solder sleeve splice (Raychem # D-1744-01) isprovided for this connection. Contact Raychem for specificinstructions on the use of this splice. Alternate splices may beused if installed in accordance with FAA AC , Section445, Splices in Electrical ELT INSTALLATION and OPERATION manual will indicate that theremote switch ground is to be connected to pin 11 of the ELT. When installing the dongle pin 11 will not be available for remoteswitch grounding. It is recommended that either the ground splice, or the aircraft grounding point mentioned in the previous paragraph be used as a remote switch DONGLE TO PREVIOUSLY INSTALLED ELT.

10 After disassembling and reassembling the 12 position rectangular ELTconnector as described in the Remote Switch/Horn Wiring sectionof this manual, there will be an unterminated ground wire from theremote switch. Ground this wire as described in the Manual570-401011 DGL-1 Manual570-4010 Aircraft AddressICAO 24 Bit AddressThe dongle will only operate with Artex ELT s that have softwareversion V133M, V134B or V135C and programmed with COSPASSARSAT 24 Bit Address Long Message Protocol. The aircraftmust have a unique 24 bit address assigned by the InternationalCivil Aviation Organization. The ICAO 24 bit address is commonlyexpressed in either an octal or hexadecimal format, and will needto be converted to binary.


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