ARTEX ELT 1000 Description, Operation, Installation And Maintenance Manual Download Page 43 | Manualshive

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ARTEX PRODUCTS / ACR ELECTRONICS, INC.

DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL

ELT 1000 (P/N: A3-06-2749-1)

Y1-03-0259 Rev. U

Company Confidential

Page 43 of 62

3)

Install a ground plane if necessary. Composite or wood airframes and fabric covered may require a ground
plane.

4)

Drill the antenna mounting holes and coax connector hole referring to the appropriate antenna illustration for
hole patterns and hole sizes. See Figure 15 below and Figure 16 below and Figure 17 on page 44.

5)

Mount the antenna referring to the appropriate antenna illustration for hardware requirements, torque, and
other applicable installation requirements.

6)

Apply a small fillet of RTV sealant around periphery of antenna base to protect against moisture.

7)

A coax cable is provided as part of some ELT kits.

Figure 15 Rod Antenna 110-338, 110-338-01 and A3-06-2835 Outlines and Dimensions

Figure 16 Blade Antenna 110-340 Outlines and Dimensions

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Summary of Contents for ELT 1000

Page 1: ... ARTEX PRODUCTS ACR ELECTRONICS INC 5757 Ravenswood Rd Ft Lauderdale FL 33312 www acrartex com ARTEX ELT 1000 Emergency Locator Transmitter Description Operation Installation and Maintenance Manual Y1 03 0259 Rev U ...

Page 2: ...pressed 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 Inc makes no warranty with regard to the documentation or data contained herein ACR Electronics Inc is not liable in the event of incidentals special consequential or any other damages in connection wi...

Page 3: ...ation 14 B Discussion 14 5 References 14 A Regulatory Documents 14 B Other Documents 15 DESCRIPTION AND OPERATION 16 1 Description 16 A Functional Overview 16 B System Components 17 2 Operation 19 A Overview 19 B Normal Operation 19 C Manual Activation 19 D ELT Reset 19 E Functional Check 19 3 Specifications 20 A Environmental and Physical 20 B Electrical 21 C Antenna 22 TEST AND FAULT ISOLATION 2...

Page 4: ...mitter Antenna Test Item 6 29 P Antenna Test Item 7 30 Q Inspection and Test Documentation Item 8 30 3 Fault Isolation 30 A Self Test 30 B Troubleshooting 32 REMOVAL 33 1 ELT 33 A ELT Removal 33 2 Battery 34 A Battery Removal 34 3 Material or Equipment Return 35 A Shipment Information 35 B Return Material Authorization 36 INSTALLATION 37 1 Regulatory Requirements and Guidelines 37 A For US Registe...

Page 5: ... I RS 232 Acceptable Nav Data 53 7 ELT Installation and Test 53 A Installation 53 B Harness ELT D Sub Plug Sealing 55 C Installation Documentation 55 8 Battery Pack Installation 55 A Battery Installation and Reinstallation 55 ILLUSTRATED PARTS LIST 57 1 Introduction 57 A Purpose 57 B IPL Usage Guide 57 2 Manufacturer Name and Address 57 A Ordering Information 57 APPENDIX A ELT REGISTRATION 61 1 Ba...

Page 6: ... D type shaped subminiature connectors connector for low voltage current signals and electrical currents DER Designated Engineering Representative An individual qualified and designated by the FAA to approve or recommend approval of technical data to the FAA 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 an...

Page 7: ...tion that makes recommendations for airworthiness refer to http www rtca org aboutrtca asp for more information RTV A rubbery silicon based adhesive typically used to prevent vibration problems and water intrusion SAR Search and Rescue SCREEN ROOM Refers to a room designed to block RF signals such that the broadcast of an ELT placed in the screen room cannot reach the SAR satellite system SERVICE ...

Page 8: ...14 Typical Mounting Tray Installation 41 Figure 15 Rod Antenna 110 338 110 338 01 and A3 06 2835 Outlines and Dimensions 43 Figure 16 Blade Antenna 110 340 Outlines and Dimensions 43 Figure 17 Whip Antenna 110 773 Outline and Dimensions 44 Figure 18 Remote Switch Outline and Dimensions 44 Figure 19 Buzzer Outline and Dimensions 45 Figure 20 Typical 2 Wire Installation for Unshielded Harness 46 Fig...

Page 9: ...ONS REVISION CHANGE DATE REVISION CHANGE DATE A W I 05 EN 05 1 25 13 B ECO 15327 3 1 13 C ECO 15360 3 21 13 C1 DECO 15369 4 2 13 D ECO 15619 5 13 14 E ECO 15619 5 13 14 F ECO 15830 12 1 14 G ECO 15937 3 19 15 H ECO 16129 9 2 15 J ECO 16173 10 23 15 K ECO 16240 1 19 16 L ECO 16440 6 30 16 M ECO 16495 9 7 16 N ECO 16503 9 14 16 P ECO 16551 12 7 16 R ECO 16575 1 18 17 U ECO 16714 7 20 17 ...

Page 10: ... INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL ELT 1000 P N A3 06 2749 1 Y1 03 0259 Rev U Company Confidential Page 10 of 62 SERVICE BULLETIN LIST SERVICE BULLETIN NO ISSUE DATE SUBJECT MANUAL REV NO MANUAL REV DATE ...

Page 11: ...aviation authority for applicable requirements B Application 1 This manual constitutes supporting data documentation for the ARTEX ELT 1000 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 the ARTEX ELT 1000 must be installed and maintained in accordance with the req...

Page 12: ... to the ARTEX web site at www acrartex com B Battery CAUTION LITHIUM BATTERY SAFETY CONCERNS INCLUDE THE POSSIBILITY OF FIRE VENTING VIOLENTLY AND VENTING OF TOXIC GASES 1 The lithium battery packs used on the ARTEX ELT 1000 are certified under TSO C142a NOTE The conditions and tests for TSO approval of this article are minimum performance standards Those installing this article on or in a specifi...

Page 13: ...O 204A in lieu of RTCA DO 160G test S C 8 0 Vibration X 9 0 Explosion Atmosphere Test Not Applicable R 10 0 Waterproofness Continuous Stream X 11 0 Fluid Susceptibility Not Applicable X 12 0 Sand and Dust Not Applicable X 13 0 Fungus Resistance Test Not Applicable S 14 0 Salt Fog Z 15 0 Magnetic Effect Test Z 16 0 Power Input Test A 17 0 Voltage Spikes Z 18 0 AF Susceptibility ZCX 19 0 Induced Sig...

Page 14: ...ertification 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 9 Maintenance Records b AC 43 210 Standardized Procedures for Requesting Field Approval of Data Major Alterations and Repairs c AC 43 9 1 Instructions for Completion of FAA Form 337 d AC 43 13 1 Acceptable Methods Techniques and ...

Page 15: ...e ARTEX model beacon programmer or beacon test set operating manuals are available from ACR Electronics Inc upon request a Document number 570 1000 453 1000 ELT Test Set Operation b Document number 570 2000 453 2000 Handheld Programmer Operations Manual c Document number Y1 03 0272 A3 06 2824 Handheld Programmer Operations Manual d Document number Y1 03 0273 A3 06 2825 ELT Test Set Operation ...

Page 16: ...is mode for 24 hours and then shut down automatically The 121 5 MHz transmitter homer transmitter will continue to operate until the batteries are exhausted which is at least 50 hours 5 The location accuracy of the 406 MHz transmitter is typically 3 km If position information is extracted from the aircraft navigation system the accuracy improves to approximately 100 meters The ELT 1000 is able to ...

Page 17: ...TEX ELT 1000 housing assembly and tray are made of high impact fire resistant polycarbonate polyester plastic see Figure 1 Figure 1 ARTEX ELT 1000 Beacon and Mounting Tray 2 The cockpit mounted remote switch assembly includes a status LED and control switch The switch allows the operator to manually activate and reset the ELT for testing see Figure 2 5 WIRE 2 WIRE Figure 2 Remote Switch Front View...

Page 18: ...uzzer provides an audible alert when the ELT is active see Figure 3 Figure 3 Buzzer 4 The battery pack for the ARTEX ELT 1000 consists of two D size Lithium Sulfur Dioxide cells see Figure 4 Figure 4 Battery Pack Assembly 5 There are 5 antennas that are used with the ARTEX ELT 1000 see Figure 5 Selection of the proper antenna is dependent upon the application Figure 5 Antennas ...

Page 19: ... activation when the aircraft is not operating The buzzer is powered by the ELT and is not dependent upon the aircraft power for operation The indicator beeps periodically with the periods between pulses increasing after 12 hours B Normal Operation NOTE The beacon will immediately begin transmitting at 121 5 MHz and will continue to do so until the ELT is deactivated or 24 hours have expired NOTE ...

Page 20: ...C Mechanical Vibration 10 g 5 Hz to 2 000 Hz Shock 500 g for 4 ms Crashworthiness 100 g for 23 ms Humidity 95 for 50 hours Penetration 55 lbs from 6 in 25 kg from 15 cm Crush 1 000 lbs 454 kg Altitude 55 000 ft 16 764 m Automatic Activation Primary G switch 4 5 0 5 ft sec 2 3 G Manual Activation Unit or remote switch Weight ELT complete w Battery Pack and Mounting Tray 1 95 lbs 0 8 kg Dimension L ...

Page 21: ...dulation 406 MHz Bi Phase L G1D 121 5 MHz Amplitude Modulation A3X Transmitter Duty Cycle 406 MHz 440 or 520 ms 1 every 50 seconds 5 121 5 MHz Continuous Peak Effective Radiated Power EIRP 406 MHz EIRP 5 W 37 dBm 2 dBm for 24 hrs 20 C to 55 C 121 5 MHz EIRP 50 mW 17 dBm for 50 hrs 20 C to 55 C Occupied Bandwidth 406 MHz 20 KHz max 121 5 MHz 25 KHz max Spurious Emissions 406 MHz Per RTCA DO 204A 12...

Page 22: ...6 MHz VSWR 121 5 MHz 2 0 1 Max 406 MHz 1 5 1 Max Polarization Vertical Monopole Radiation Pattern Omnidirectional Impedance ohms 50 Nominal Weight 0 45 lbs 0 20kg 0 18 lbs 0 08 kg 1 40 lbs 0 64 kg 0 45 lbs 0 20kg Coax Cable RG 142 or RG 400 0 5dB 1 dB Insertion Loss Connector BNC Female Dimensions Base to Tip 15 5 in 394 mm 15 in 381 mm 7 75 in 197 mm 15 5 in 394 mm Table 4 Antenna Specifications ...

Page 23: ...n insecure mounting and improper operation NOTE ARTEX recommends using www 406Test com to ensure the ELT 1000 is testing through the satellite during annual inspections and initial installations B Canada 1 CAR Part VI Standard 625 Appendix C requires the ELT to be inspected at intervals not exceeding 12 months 2 All maintenance and testing shall be performed in accordance with the requirements of ...

Page 24: ...requency Measurement 5b Audio Modulation Check 5c 121 5 MHz Power Output Measurement 5d 406 MHz Frequency Measurement 5e 406 MHz Power Output Measurement 5f Current Draw Test 5g Digital Message Verification 5h ELT Reset Check 6 Installed Transmitter Test 7 Antenna Test 8 Inspection and Test Documentation Table 5 ELT Inspection Checklist B Preparation 1 Remove the ELT See Figure 9 on page 33 for in...

Page 25: ...t activation of unknown duration c When the total of all known transmissions exceeds one hour d On or before battery replacement expiration date NOTE The new expiration date for replacing the battery must be legibly marked on the outside of the transmitter and entered in the aircraft maintenance record F G Switch Functional Check Item 4 1 Reinstall the battery in accordance with Figure 28 on page ...

Page 26: ... an RF enclosure or screen room to prevent RF emissions 3 For final airworthiness verification use the ELT s own battery pack as the power source for these measurements An alternate power source can be used where lengthy servicing other than the performance tests is anticipated Expired battery packs can be used if the airworthiness performance of the battery pack in the system is not required The ...

Page 27: ... ELT product label K 406 MHz Power Output Measurement Item 5e CAUTION POWER OUTPUT IS APPROXIMATELY 5 WATTS BE SURE ADEQUATE ATTENUATION IS INSERTED BETWEEN THE ELT AND THE MEASURING INSTRUMENT 1 Connect the measuring device as specified in Figure 6 Performance Test Setup on page 26 2 Activate the ELT if necessary by placing the control switch in the ON position 3 Wait three minutes 4 Read the dis...

Page 28: ...TION THE NEXT MEASUREMENT COULD CAUSE THE INTERNAL PROTECTION FUSE OF THE AMMETER TO BLOW IF PRECAUTIONS ARE NOT OBSERVED 7 Set the ammeter current range to accommodate 4A amp 8 Activate the ELT 9 Allow ELT to transmit a 406 MHz burst This will occur 50 seconds after activation 10 Set the ammeter to read approximately 60 mA of current 11 Observe reading Current shall be 55 mA 12 Deactivate the ELT...

Page 29: ...xamples N ELT Reset Check Item 5h 1 Place the ELT control switch in the ON position 2 Return the switch to the ARM position 3 If the ELT is working properly the LED will turn off O Installed Transmitter Antenna Test Item 6 1 Re install the ELT in Aircraft 2 Perform the following functional check within the first 5 minutes after the hour UTC as required by AC 43 13 1 Chapter 12 12 22 Note 3 3 Notif...

Page 30: ...ogbook including the date the ELT inspection and testing was satisfactorily completed 2 For aircraft operating under Canadian authority following satisfactory completion of performance testing the date on which the test was performed shall be marked on the ELT external casing in a legible and permanent manner 3 Fault Isolation A Self Test 1 The self test checks certain critical functions in the be...

Page 31: ...k coax cable and connectors for shorts and opens bad center pin etc Disconnect then reconnect cable Repeat self test 4 Check antenna ground for low resistance should be 100 m Ω 5 Antenna should be 3 away from any vertical metal 6 Have antenna checked by factory 5 No position data present long message protocol only Error is suppressed for short messages Aircraft navigation system OFF Turn on naviga...

Page 32: ...ircuit Verify integrity of all crimp and solder connections ELT will not turn off Turn ELT OFF using local switch If ELT turns off Defective remote switch harness reset circuit wiring Check wiring continuity and repair as necessary Defective remote switch Replace remote switch If ELT does not turn OFF using local switch ELT defective Remove battery pack to disable ELT and return ELT to factory for...

Page 33: ...e NOTE Check the coax cable center conductor pin which is prone to retracting into the connector housing 3 Remove remote switch harness D sub plug 4 Open the metal strap NOTE 1 When opening the metal strap use caution to avoid pinching your fingers in the latch A flat screwdriver can be placed under the latch to spring it open if needed NOTE 2 Never open the strap by prying it open from the top On...

Page 34: ... Battery Removal CAUTION THE BATTERY PACK CONTAINS ELECTROSTATIC DISCHARGE ESD SENSITIVE COMPONENTS AND IT MUST BE HANDLED WITH CARE IF POSSIBLE WEAR A GROUNDED WRIST STRAP WHEN HANDLING THE BATTERY PACK DURING INSTALLATION ACTIVITIES TAKE PARTICULAR CARE TO AVOID TOUCHING THE EXPOSED CIRCUIT BOARD AND CONNECTOR PINS ON THE BOARD CAUTION TAKE CARE NOT TO DAMAGE THE SHORT FLEX CABLE WHICH CONNECTS ...

Page 35: ...he ELT taking care not to put strain on the short flex cable 6 Disconnect the flex cable from the small circuit board mounted in the battery pack by carefully opening the flex cable connector 7 Dispose of battery within the rules and guidelines of your regional Waste Disposal Authority 3 Material or Equipment Return A Shipment Information 1 If any material or equipment is to be returned to the fac...

Page 36: ...aul ACR Electronics Inc 5757 Ravenswood Road Fort Lauderdale FL 33312 6645 USA Phone 954 981 3333 Fax 954 983 5087 a Failure to obtain a RMA number and provide the details listed above 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 retur...

Page 37: ...1 TSO approval of the ELT does not constitute installation approval All ELT 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 2 The remote switch is a requirement of TSO C126a and installation is mandatory 3 The buzzer is a requirement of TSO C12...

Page 38: ... 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 c...

Page 39: ...E EXTREMELY RIGID MOUNTING AN ELT DIRECTLY TO THE AIRCRAFT SKIN FOR EXAMPLE IS UNACCEPTABLE CAUTION AVOID LOCATING THE ELT WHERE IT WILL BE SUBJECTED TO UNPROTECTED EXPOSURE TO HARSH CHEMICAL FLUIDS SUCH AS DEICING COMPOUNDS THESE TYPES OF CHEMICAL FLUIDS CAN PROMOTE CRACKING AND FRACTURING OF THE ELT MOUNTING FRAME AND HOUSING COMPONENTS BY DEGRADING THE STRUCTURAL INTEGRITY OF THESE COMPONENTS T...

Page 40: ...rance Dimensions 1 Select a suitable location for the ELT mounting tray see Figure 12 ARTEX ELT 1000 Outline Dimensions on page 39 and Figure 13 ELT 1000 Metal Strap Minimum Clearance Dimensions above 2 Mount the ELT as far aft as practical but where it can be easily retrieved for maintenance 3 Additional installation guidance may be found in AC 43 13 2 Chapter 2 28 which specifically addresses EL...

Page 41: ...the arrow on the tray is within 10 of the longitudinal axis of the aircraft and pointing in the direction of flight 4 Mark and drill the four mounting holes with a 19 or 4 25 mm drill Refer to Figure 12 on page 39 for the mounting hole pattern 5 Install the mounting tray as shown in Figure 14 installation kit 455 7423 NOTE The use of substitute mounting hardware is acceptable provided the hardware...

Page 42: ...r class of aircraft must determine that the aircraft installation conditions are within the TSO standards TSO articles must have separate approval for installation in an aircraft CAUTION ARTEX CANNOT VERIFY APPROPRIATE ANTENNA SELECTION PER EACH AIRFRAME MANY CONSIDERATIONS MUST BE EVALUATED DURING THE ANTENNA SELECTION PROCESS SUCH AS DYNAMIC STATIC LOADING CERTAIN SPECIAL CONSIDERATIONS NEED TO ...

Page 43: ...ropriate antenna illustration for hole patterns and hole sizes See Figure 15 below and Figure 16 below and Figure 17 on page 44 5 Mount the antenna referring to the appropriate antenna illustration for hardware requirements torque and other applicable installation requirements 6 Apply a small fillet of RTV sealant around periphery of antenna base to protect against moisture 7 A coax cable is provi...

Page 44: ...switch and notice the indicator LED 2 The switch assembly requires a panel area of approximately 2 0 x 1 3 in 51 x 33 mm Figure 18 shows the dimensions The clearance behind the panel must allow for the mating connector and harness wires as well as the switch depth Figure 18 Remote Switch Outline and Dimensions B Installation 1 Mark the cutout on the cockpit panel 2 Fit the switch assembly into the...

Page 45: ...OCKPIT 1 Select a suitable location for the buzzer NOTE The buzzer may be located anywhere in the aircraft however the recommended location is near the ELT as the buzzer is loud enough to be heard outside the aircraft when the engine s is not running When the engine s is running the LED on the cockpit remote switch assembly will warn the pilot the ELT is active B Installation 1 Refer to AC 43 13 2...

Page 46: ...MAGE DO NOT CONNECT THE HARNESS TO THE ELT OR COCKPIT REMOTE SWITCH UNTIL ALL POWER AND GROUND WIRING CONNECTIONS ARE COMPLETED AND VERIFIED 1 The following wiring and grounding 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...

Page 47: ... ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL ELT 1000 P N A3 06 2749 1 Y1 03 0259 Rev U Company Confidential Page 47 of 62 Figure 21 Typical 2 Wire Installation for Shielded Harness ...

Page 48: ... ACR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL ELT 1000 P N A3 06 2749 1 Y1 03 0259 Rev U Company Confidential Page 48 of 62 Figure 22 Typical 5 Wire Installations for Metal Airframes ...

Page 49: ...CR ELECTRONICS INC DESCRIPTION OPERATION INSTALLATION AND MAINTENANCE MANUAL ELT 1000 P N A3 06 2749 1 Y1 03 0259 Rev U Company Confidential Page 49 of 62 Figure 23 Typical 5 Wire Installations for Composite Airframes ...

Page 50: ... cable wires Dress and tin the bare wires to prevent the strands from fraying during terminal crimping operations 4 Support for the harness wiring can be referenced in AC 43 13 1 Chapter 11 9 through 12 5 Install the buzzer connecting wires NOTE The buzzer ground and the ELT ground must be common The buzzer ground can be connected directly to the ELT D sub ground 6 For 5 wire remote switch install...

Page 51: ...und pin for composite airframe installations see Figure 21 Typical 2 Wire Installation for Shielded Harness on page 47 Figure 23 Typical 5 Wire Installations for Composite Airframes on page 49 for composite airframe wiring diagrams 6 Solder a short jumper wire G switch loop between pins 5 and 12 of the harness connector CAUTION THE ELT WILL NOT AUTOMATICALLY ACTIVATE IF THE JUMPER G SW LOOP IS NOT...

Page 52: ...ames on page 49 NOTE Terminal pins may be removed from the plug using Molex extraction tool 11030002 or equivalent E Antenna Connection 1 Install the coax cable to the antenna A custom length coax cable up to 20 feet 6 m may be fabricated if the cable provided is not adequate ACR suggests using RG 142 or RG 400 coax cable F Cockpit Remote Switch Power Connection 1 For 5 wire remote switch installa...

Page 53: ...external navigation data if available 2 ELTs programmed with SHORT Cospas Sarsat protocol will not accept navigation data 3 When the ELT 1000 is programmed with 4800 baud it will only accept NMEA and when programmed with 9600 baud it will only accept Aviation Protocol I RS 232 Acceptable Nav Data 1 NMEA 0183 baud rate is 4800 2 Aviation protocol baud rate is 9600 3 Programing of the ELT 1000 will ...

Page 54: ... through the strips 5 Connect the harness to the ELT taking care to insert the connector straight in Secure the connector with the thumbscrews NOTE Care must be taken in the cable connection process to avoid shorting any pins to ground or each other Under some circumstances the shorting or grounding of the pins signal the ELT as if the remote switch was activated This may result in ELT transmissio...

Page 55: ...ptacles lightly with sealant f Re connect the harness plug to the ELT C Installation Documentation 1 Update logbook aircraft records entries and submit FAA Form 337 along with any supporting data required by the FAA for approval of the installation as applicable 2 In countries other than the United States make appropriate aircraft records entries and submit documentation as required for installati...

Page 56: ...lug on the battery pack circuit board using the other hand taking care not to put a twist in the flex cable NOTE The receptacle should click into place when properly mated to the plug If the ELT activates when power is connected reset by toggling the ELT local control switch to ON and back to ARM after 1 2 seconds 7 Fit the battery pack into place on the ELT making sure the gasket is positioned co...

Page 57: ...e the item number assigned to the part c Refer to the associated parts list and find the item number in the Fig Item column 2 If the part number is known a Refer to the parts list and find the part in the Part column b Note the figure number and item number assigned to the part c Refer to the illustration in the applicable IPL figure to find attaching hardware and related assembly parts 3 In cases...

Page 58: ... PART DESCRIPTION QTY A3 06 2749 1 ARTEX ELT 1000 Final Assembly 1 01 A3 06 2748 1 ARTEX ELT 1000 Main Assembly 1 03 452 6504 1 Lithium Battery Pack 1 04 183 0050 Gasket 0 093 x 0 055 1 05 201 0402 Screw 6 32 x 7 8 PHL Truss SS 8 06 A3 06 2758 1 Mounting Tray 1 201 0810 Screw PHL 8 32 x 5 8 SS 4 246 0008 Washer Flat SS 8 4 241 0832 Nut Hex 8 32 x SS 4 A1 20 1671 Label LiSO2 ARTEX ELT 1000 1 Table ...

Page 59: ...crew PHL 4 40 x SS 4 247 0400 Washer internal lock SS 4 4 241 0440 Nut 4 40 x hex SS 4 591 0428 Label ELT Cautionary Use Advisory 1 151 5009 Plug 9 pin 1 151 6628 Terminal crimp female 0 062 dia 4 02 150 1130 Conn D sub 15 pin Female Solder cups 1 03 150 1127 Housing D sub 15 pin grommet thumbscrews 1 850 0814 Sealant strip D sub connector 2 201 0810 Screw PHP 8 32 x 5 8 SS 4 241 0832 Nut 4 246 00...

Page 60: ...2 Figure 31 Antennas ITEM PART DESCRIPTION QTY 01 110 338 01 Antenna Rod CI317 1 black single input 1 02 110 773 Antenna 121 5 406 MHz whip 1 03 110 340 Antenna Blade 1 04 A3 06 2835 Antenna Rod CI315 1 white single input 1 05 110 338 Antenna Rod CI317 1 white single input 1 611 6013 04 Cable coax BNC to BNC 6 1 611 6013 13 Cable coax BNC to BNC 12 1 Table 10 Antennas ...

Page 61: ...t aircraft i e an aircraft other than the one it was originally installed on and or the aircraft is registered in a new country the ELT must be re programmed and re registered b If the aircraft is registered in a new country the ELT must be re programmed and re registered c The product label must be re marked with the new HEX ID code to indicate new programming if applicable B Required Information...

Page 62: ...y Confidential Page 62 of 62 NOTE NOAA may also be contacted by mail at SARSAT Beacon Registration NSOF E SPO53 1315 East West Hwy Silver Spring MD 20910 9684 or by phone at 1 888 212 7283 or 301 817 4565 3 In other countries the national civil aviation authority in the applicable country should be contacted to obtain registration information ...

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