USER'S HANDBOOK INCLUDING INSTALLATION MANUAL
Contents
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3. SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool REPAIRL_ REPAIRL_ Appendix B page 9 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING EE MM YYYY DATE fats filiis MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY sERviciNGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE ftue MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool REPAIRL REPAIRL_ Appendix B page 10 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING EE MM YYYY DATE fats filiis MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY sERviciNGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE ftue MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the R
4. 18 22 Page 9 Feb 15 03 R n Say w ELTR USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK Page 10 BLANK h x ELTA USER S HANDBOOK 1 INTRODUCTION TO THE COSPAS SARSAT SYSTEM A The COSPAS SARSAT system The purpose of the COSPAS SARSAT satellite system is to detect and locate all distress signals transmitted by aeronautical maritime or land based beacons for the search and rescue organizations This program is the result of an international collaboration between the United States Canada and France on the one hand SARSAT project and Russia on the other hand COSPAS project These two projects are fully compatible Since the first results were obtained several countries have joined the program Several other countries have shown an interest and will soon be joining the COSPAS SARSAT system partners ELTA in relation with CNES French National Space Agency has developed the complete range of products required for COSPAS SARSAT system operation Following an in depth study phase ELTA has arrived at highly conclusive technical results and experimental and operational use of the ground equipment have proven this equipment s reliability and ease of use B System organization Ref Fig 1 In the COSPAS SARSAT system space equipment is placed on board several satellites in low near polar orbit to capture transmissions from emergency transmitters and to retransmit these signals to specialized ground statio
5. Connect the remote control unit cable to the REMOTE CONTROL connector on ELT and lock it Connect the remote control unit cable rear of the remote control panel and lock it Switch the Beacon ARMED OFF ON lockable toggle switch to ARMED pull and slide the system is ready for use Note the beacon can be used in automatic mode with neither RCP nor external antenna CAUTION AS SOON AS THE BEACON IS IN ARMED IT CAN BE AUTOMATICALLY ACTIVATED BY THE INTERNAL G SWITCH 2 Installation in survival mode Connect the whip back up antenna to ELT The switch shall be on OFF Page 28 Feb 15 03 h x ELTA USER S HANDBOOK 5 UTILIZATION OF THE ELT ADT 406 AP Ref Fig 7 CAUTION IN THE EVENT OF UNTIMELY BEACON ACTIVATION SHUTDOWN THE BEACON AND INFORM THE CLOSEST SEARCH AND RESCUE SAR OR AIRPORT CONTROL TOWER IMMEDIATELY The ELT ADT 406 can be activated in two modes automatic when the acceleration sensor is triggered manual A Automatic activation The acceleration sensor has detected an impact sufficient to trigger it The indicator light 11 and the aural indicator indicate beacon activation If the aircraft has to be evacuated refer paragraph B 2 second case Otherwise do not do anything and leave the beacon in operation until the rescue team arrives B Manual activation There are two cases in which a distress signal may be triggered manually the acceleration sensor G switch has not
6. REPAIRL REPAIRL_ Appendix B page 13 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING EE MM YYYY DATE fats filiis MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY sERviciNGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE ftue MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool REPAIRL REPAIRL_ Appendix B page 14 Feb 15 03
7. 03 18 Apr 17 03 19 Feb 15 03 20 Apr 17 03 21 Feb 15 03 22 Feb 15 03 23 Feb 15 03 24 Feb 15 03 25 Feb 15 03 26 Apr 17 03 27 Apr 17 03 28 Apr 17 03 29 Apr 17 03 30 Apr 17 03 31 Apr 17 03 32 Apr 17 03 33 Feb 15 03 34 Feb 15 03 35 Apr 17 03 Page 3 May 16 14 R Ga Nu ELTR USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK Page 4 BLANK Figure 1 Figure 2 Figure 3 Figure 4 Figure 5 Figure 6 Figure 7 h b ELTR USER S HANDBOOK TABLE OF ILLUSTRATIONS COSPAS SARSAT System Principle ELT ADT 406 AP Presentation ELT ADT 406 AP Dimensions Basic Configuration Tolerances on the Axis for Installation of the ELT ADT 406 AP Installation of the ELT ADT 406 AP Drilling Pattern Dimensions ELT ADT 406 AP Installation Wiring Diagram ELT ADT 406 AP Detailed Description Page 12 14 15 22 24 26 34 Page 5 Feb 15 03 R n Say w ELTR USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK Page 6 BLANK CAUTION 1 CAUTION 2 CAUTION 3 CAUTION 4 CAUTION 5 h ELTA USER S HANDBOOK LEADING PARTICULARS THIS TRANSMITTER IS AUTHORIZED FOR USE ONLY DURING SITUATIONS OF GRAVE AND IMMINENT DANGER IT IS IMPERATIVE THAT EACH BEACON OWNER REGISTERS THEIR BEACON CONTACT ELTA OR APPROVED AGENT TO OBTAIN THE INFORMATION RELATIVE TO THIS REGISTRATION THE BEACON MUST IMPERATIVELY BE PROGRAMMED WITH THE RELEVANT IDENTIFICATION AUTHORIZED BY THE LOCAL AIRWORTHINESS
8. ADT 406 AP Drilling Pattern Dimensions Figure 5 Page 24 Feb 15 03 h x ELTA USER S HANDBOOK C External antenna installation This antenna should be approved by ELTA ELTA recommend to use P N 25988 antenna model 2624 82 manufactured by CHELTON The external antenna must be installed on the upper part of the fuselage as far aft as possible Particular care must be taken with this attachment Standart industry means must be used to lock the screws The contact surface should be reinforced to prevent the antenna from tearing away at high speeds The cable used shall be of a high quality with very low losses RG 142 cable type is recommended with a length lower than 2 meters to keep losses close to 0 5 dB Connect the connector to the antenna and to the EXT ANT access on ELT and install the coaxial cable This cable must be fixed to rigid aircraft structure all along its routing and it should be as short as possible to avoid Radio Frequency losses and or cable destruction in case of crash D Remote control unit installation The ELT ADT 406 AP can be remotely controlled by using a remote control panel installed in the cockpit of the aircraft The maximum length of this link is 200 meters and requires no grounded cable The link requires 4 wires Page 25 Feb 15 03 h x ELTA USER S HANDBOOK The following simplified diagram shows the wiring between the ELT ADT 406 AP and its peripherals The Remote
9. JON IVAO IddV LVSUVS SVdsOO z Svdsoo Feb 15 03 Appendix page 1 JTSO 2C91a AND JTSO 2 126 APPROVAL s Fratecoied LIQUE FRAN AISE DIRECTION GENERALE DE L AVIATION CIVILE Membre des Joint Aviation Authorities JOINT TECHNICAL STANDARD ORDER AUTHORISATION Num ro F O 112 Number Conform ment la r glementation nationale en vigueur et dans les conditions indiqu es ci apr s la Direction G n rale de l Aviation Civile en accord avec les proc dures JAA concernant le autorisations JTSO atteste par le pr sent certificat que Pursuant to the national regulations for the time being in force and subject to the conditions specified below the Direction G n rale de l Aviation Civile i in accordance with JAA procedures for JTSO Authori sation hereby certifies ELTA 14 Place Marcel Dass ULT 31702 BLAGN CEDEX F 6 029 15 12 98 est autoris d identifier jes articles ci d sous par Te s marquage s JTSO indiqu s pour is authorised to identify the following article s with fe JTSO marking s for Modele D signation JT REDA tri fr quences Auto Portable et Survie ADT 406 AP 9 x Portable amp Survival tri frequency automatic ELT 2 JTS 91 JFSO 2C126 ADT 406 AP ADT 406 AP CONDITIONS 1 Le d tenteur de cette autorisation JTSO ne peut identifier son qu
10. MHz and 243 MHz signals which enable the final approach of the rescue teams in homing mode Information reliability the structure of the digital signal transmitted by these beacons makes it possible to be sure that there is actually a distress situation as well as to identify automatically the mobile in distress which is vital for rescue operations Unique identification each beacon has it s own identification information D ELTA andthe COSPAS SARSAT system 1 406 MHz distress beacons These beacons transmit to the satellites a digital message which identifies them and gives their position as well as a signal that facilitates the final approach of the rescue teams They are suitable for all types of use maritime aeronautical and land and can depending on the model be activated manually or automatically They are designed to function in the most extreme conditions with a high degree of reliability 2 Satellites low earth orbiting At least four satellites are permanently operational Since their orbit is near polar in the worst case every point on Earth is overflown every two hours In a ground station s visibility zone the satellites directly transmit the messages captured in that zone and also any messages from the zones not covered that they have stored in memory 3 Geo stationary satellites are now available in the system and offer faster detection capability close to 5 minutes but require a GPS receiver to supply
11. ONCE THE BEACON HAS BEEN PROGRAMMED IT IS GENERALY ASSIGNED TO AN AIRCRAFT NAME AND IDENTIFICATION IF THIS BEACON IS USED ON ANOTHER AIRCRAFT IT WOULD HAVE TO BE REPROGRAMMED NEW NAME AND IDENTIFICATION BEFORE INSTALLING OR USING THIS EQUIPMENT THE VALIDITY OF THE INFORMATION ON THE BEACON LABEL MUST IMPERATIVELY BE CHECKED Page 7 Feb 15 03 R n Say w ELTR USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK Page 8 BLANK h x ELTA USER S HANDBOOK TABLE OF CONTENTS 1 INTRODUCTION TO THE COSPAS SARSAT SYSTEM A The COSPAS SARSAT system B System organization C The distress frequencies D ELTA and the COSPAS SARSAT system 2 GENERAL DETAILS OF THE ELT ADT 406 AP A Purpose of the ELT ADT 406 AP B Characteristics 3 DESCRIPTION OF THE ELT ADT 406 AP AND OF THE AIRCRAFT COMPONENTS A General description B Detailed description 4 INSTALLATION OF THE ELT ADT 406 AP A General B Installation of the beacon on the aircraft C External antenna installation D Remote control unit installation E Installation and configuration of the beacon 5 UTILIZATION OF THE ELT ADT 406 AP A Automatic activation B Manual activation C Beacon shutdown D Beacon self test 6 MAINTENANCE THE ELT ADT 406 A Beacon self test B Maintenance periodicity table C Battery replacement D Battery discarding E Test to do at the time of a beacon return in workshop 14 14 16 18 18
12. Test to do at the time of a beacon return in workshop Perfoms the following tests described in CMM 25 60 10 visual check test of acceleration sensor automatic triggering functional test of ADT 406 AP beacon RF test on the operational frequencies 121 5 243 406 MHz Page 34 Feb 15 03 h x ELTA USER S HANDBOOK 2 FRONT FACE 3 ACTIVATION IDENT ASSY 4 BACK FACE 5 MACHINED SECTION 6 STRAP 7 FLOAT 8 SUPPORT 9 EXT ANT BNC CONNECTOR FEMALE 10 REMOTE CONTROL CONNECTOR FEMALE HD 15 PINS 11 TX LED 12 ARMED OFF ON TOGGLE AND GUARDED SWITCH 13 BACK UP ANT TNC CONNECTOR FEMALE 14 METALIC STRAP ELT ADT 406 AP Detailed Description Figure 7 Page 35 Apr 17 03 COSPAS SARSAT TYPE APPROVAL CERTIFICATE prepuris paoiddyr 2451 15305 50507 o quas oouvpiooos ur Pojelisuoutop oosugturono d 3591165 pue uoxe USSG SEY UOTJOT ANIMO A10109JSD9S ponssi Aew 950192 Mott worpoyicsds 125TeG SE SOI 15901 aseos PONSSI St Joy oed y uoopoq poys pouncs yesmeg sedsog oui Aq 51 ST6STJIMOSISIUT L N SIU snsmu JO 90ULUSSI SU UHA o 1no Suisue Aygen pue Aue lt sso3dxo 35105 50505 pue Aum e JOU SI oyeorgn1oo STUL UISIS S 1 ou thua asn 1
13. of approximately 6 second the self test is displayed on the Remote Control Unit LED 10s permanent illumination for correct operation 10s blinking condition for failure detection Blinking rate indicates the failure source detection as follow 125 ms ON 125 ms OFF Frequency 4 Hz ELT Check Sum failure software problem 250 ms ON 250 ms OFF Frequency 2 Hz ELT power failure UHF and or VHF 500 ms ON 500 ms OFF Frequency 1 Hz Ext Antenna connection failure or signal identification missing NOTE On the beacon after the two short blinks the indicator light 11 comes ON and the buzzer sounds during 6 seconds This is the self test process Then the self test report is indicated as it is done for the Remote Control Unit LED CAUTION THE ELT SHALL BE IN ARMED POSITION IF NOT REMOTE CONTROL WILL NOT OPERATE TEST RESET ON Page 32 Apr 17 03 h x ELTA USER S HANDBOOK 6 MAINTENANCE THE ELT ADT 406 A Beacon self test The manufacturer recommends that a beacon self test should be performed regularly The highest rate is one per day Normally this task is added to other periodic maintenance task such a A check In all events the user must comply with the applicable regulations in the country concerned governing the self test period The self test must only be performed when the order to do so is given or by the competent authorities A higher rate of self test will reduce the 5 years
14. until surrendered withdrawn or otherwise tertuinated by the FAA FAR 21 621 The FAA may upon notice withdraw the letter of TSO design approval of any manufacturer who identifies with a TSO marking any article not meeting the performance standards of the applicable TSO FAR 21 619 The DGAC France airworthiness certification is essential to the determination that the item meets the performance standards of the applicable TSO If there are any questions please feel free to have your staff contact Gregory A Edwards Tel 322 508 2714 Sincerely Thomas A Boudrcan Manager Aircraft Certification Staff FAA Brussels Reference GE vk 06 12 03 0073 03 page 4 sb 15 03 295 dj 90 LI H 1 spueg 1891 to EO gO 10 77 qo E JjJ SHL ON EMO E EN n Sd4 OS AV 1 L S I GJAIHJA JAUNO is ose 1 GNV8 JONVHITOL gt k P eeaoret ere eee j SIHL NI l ui SNOILVH31390V JO NOU VNIBWOO t ANY 311VALLOV 1SNN HOSNIS Fen pun N Mt S42 O y 9 WOH4 OJAIHJA 3Auno SI 06 Ge 9 NOLLVH3 1200V Crash Sensor Response Curve Appendix A page 5 Feb 15 03 LOG BOOK FACTORY SETTING NEXT BATTE
15. Control Panel in cockpit identified as RCP the external antenna noted as EA the whip antenna noted as BA The EA is connected to the ELT ADT 406 AP BNC female connector 5 The BA is connected to the ELT ADT 406 AP TNC female connector 1 The RCP is connected to the ELT ADT 406 AP high density 15 pins female connector 3 ELTA recommend to use P N 16243 for RCP connector and P N 231 plus 232 for ELT A three position guarded switch 2 controls the ELT ADT 406 AP A red indicator 4 displays the ELT ADT 406 AP state RCP P N 93N6035 as example EA P N 25988 recommended ET ON TEST RESET 4 wires not supplied omen ELT HD 15pt RCP BA P N 02N69004 CONNECTOR CONNECTOR 50 ohms coaxial cable ON ARMED 1 E not supplied ELT ACTIVATED 5 C male connector TEST RESET 7 D V 13 406 ADT 406 AP Beacon Installation Page 26 Apr 17 03 n en N ELTA Figure 6 Page 27 Apr 17 03 h x ELTA USER S HANDBOOK E Installation and configuration of the beacon Ref Fig 5 1 Installation in automatic mode CAUTION TO BE OPERATIONAL THE BEACON SHALL BE IN ARMED POSITION ONCE IT HAS BEEN CORRECTLY INSTALLED Connect the antenna cable to the EXT ANT connector Switch the Remote Control ON ARMED lockable toggle switch to ARMED on remote control panel
16. F test sheet issued from the ELTA test tool REPAIRL REPAIRL_ Appendix B page 11 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING EE MM YYYY DATE fats filiis MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY sERviciNGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE ftue MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool REPAIRL REPAIRL_ Appendix B page 12 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING EE MM YYYY DATE fats filiis MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY sERviciNGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE ftue MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool
17. Hz 243 MHz CLASS 2 20 55 C el n ELTA F6614 FRANCE www elta fr WARNING THIS TRANSMITTER IS AUTHORIZED FOR USE ONLY DURING SITUATIONS OF GRAVE AND IMMINANT DANGER AVERTISSEMENT CET EMETTEUR NE DOIT ETRE UTILISE QU EN SITUATION DE DANGER GRAVE ET IMMINENT APPROVAL NUMBER JTSO 2C91a amp 2C126 N HOMOLOGATION TSO C91a amp C126 PIN 01 65910 REV A b Connectors use label This label gives indication on the electronic front face connectors use PORTABLE MODE MODE PORTABLE MANUAL MODE UNLOCK CONNECTORS o PULLSWITCH REMOVE CABLES MOVE TO ON o DEVERROUILLER LES CONNECTEURS 90 TIRER L INTERRUPTEUR RETIRER LES CABLES o PLACER SUR ON MODE MANUEL AUTOMATIC MODE MODE AUTOMATIQUE PULL SWITCH AND MOVE TIRER LINTERRUPTEUR TO ARMED PLACER SUR ARMED PN 03N60425 Page 19 Feb 15 03 h x ELTA USER S HANDBOOK c Connectors location label This label indicates the location of the connectors on the front face of the electronic assy BACK UP ANT REMOTE CONTROL EXT ANT SWITCH OFF FOR MAINTENANCE d ldentification label This label indicates the axis according to which the ELT ADT 406 AP must be installed on the aircraft see paragraph 4 B for automatic activation G switch It is fixed to the activation identification module DIRECTION OF FLIGHT Homing pwr xx dBm __ Homing power Of
18. OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool Appendix B page 6 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encodin
19. R PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool Appendix B page 4 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool Appendix B page 5 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN
20. RY SERVICING _ MM YYYY Appendix B page 1 Feb 15 03 LOG BOOK FACTORY SETTING Appendix B page 2 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool Appendix B page 3 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBE
21. The beacon is integrated in the aircraft as far aft as possible and so it must be connected to the remote control unit This remote control unit enables beacon operation to be forced to ON to be tested TEST or shutdown and restore in standby or ARMED mode RESET in the event of an untimely triggering of the ELT from the aircraft cockpit h External antenna An external antenna is recommended to be installed on the fuselage of the aircraft to maximize transmission of the distress signal to the satellites The cable lenght should remain as short as possible in order to RF keep losses as close as possible to 0 5 to 1 dB at each frequencies 121 5 243 406 028 MHz Page 21 Feb 15 03 h x ELTA USER S HANDBOOK 4 INSTALLATION OF THE ELT ADT 406 AP A General System security and reliability obviously depends on the standard of installation In order to ensure installation of the highest standard the installation operations must be performed in conformity with this document performed in compliance with the current regulations performed by qualified personnel performed so that the aircraft s structural integrity is not affected it will not hinder the pilot in normal position it will not cause any damage in the event of an accident it will not prevent or modify operation of the other safety systems If in doubt contact the aircraft manufacturer or its representative inspected by representative authority B Ins
22. ation direction is selectable 4 possibe directions color orange conformity with the international distress signal self test transmission of one burst modulated with inverted frame synchronization and 5s transmission of 121 5 MHz automation to off position on remote control panel any COSPAS SARSAT protocol available ELTS N A C operator designator and S N A C 24 bits address A C nationality and registration marking recommended Test any country code available can operate in short or long C S message For long message location data from on board GPS as exemple is received from A C data bus through an interface module P N 01N6593 x C S identification stored in a transferable module to ease maintenance on ELT dual antenna access Primary for external antenna and back up antenna in case of failure detection on primary access Page 17 Apr 17 03 h x ELTA USER S HANDBOOK DESCRIPTION OF THE ELT ADT 406 AP AND OF THE AIRCRAFT COMPONENTS A General description 1 Introduction This beacon from the ADT406 family derives from the ADT 406 AF AP model Consequently this beacon features the functional capabilities of the AF AP besides its flotation gear the attachment interface and its flexible antenna entirely compatible with Cospat Sarsat 2 The ELT ADT 406 essentially consists of anADT 406 AP beacon transmitter awhip antenna labels an activation ide
23. battery servicing CAUTION THE SELF TEST PROCEDURE PARAGRAPH 5 D MUST BE RESPECTED TO AVOID UNTIMELY BEACON ACTIVATION B Maintenance periodicity table Periodicity Operations Operator 5 years Replacement of batteries ELTA or approved agent airline General overhaul in specialized workshop ELTA or approved agent airline 5 years C Batteries replacement CAUTION THE BATTERY PACK SHALL BE APPROVED BY ELTA IF OTHER PACK ARE USED ELTA WILL CANCEL WARRANTY AND WILL REFUSE ANY RESPONSIBILITY ON THE PRODUCT OPERATION MISFUNCTION CAUTION THE BATTERIES USED CANNOT BE RECHARGED DO NOT TRY TO OPEN OR RECHARGE THEM Next battery servicing date is indicated on a label stuck on the back face of ADT 406 AP The old batteries must be replaced with new batteries of a model approved by ELTA P N 02N60052 battery servicing for one ELT or 02N60053 battery servicing for ten ELTs ELTA recommends that the ELT ADT 406 AP should undergo a general overhaul on its test and programming bench at this occasion Refer to CMM 25 60 10 for detail of operation Page 33 Feb 15 03 h x ELTA USER S HANDBOOK D Batteries discarding The batteries must be discarded in compliance with the applicable regulations in the country concerned NOTE The type of battery used is not dangerous for the environment provided that it is completely discharged Contact ELTA for getting additional discarding information E
24. been triggered but a distress signal must be sent injured passengers aircraft out of operation the aircraft is on the ground and must be evacuated 1 First case from the Remote Control Raise the safety cover guard on the remote control unit and place the switch in the ON position lever upwards An automatic self test sequence is performed Then the indicator light 11 and the aural indicator indicate beacon activation This signal is permanently displayed on the Remote Control LED Do not do anything and leave the beacon in operation until the rescue team arrives 2 Second case from the beacon Place the beacon switch 12 in the ON position pull and slide An automatic self test sequence is performed Then the beacon enter in a waiting condition for about 30s This state is displayed by flashing on indicator light 10 1 75 s ON 0 25 s OFF This delay will avoid unwanted activation false manoeuvre Then the indicator light 11 and the aural indicator indicate beacon activation The actual distress signal is transmitted This state is displayed by flashing on indicator light 0 5 s ON 0 5 s OFF Page 29 Apr 17 03 h x ELTA USER S HANDBOOK If the aircraft has to be evacuated Follow the instructions unfasten the strap and the cable if relevant remove the beacon from its bracket pull firmly to brake the retaining metallic strap 14 Ref Fig 7 extend the ant
25. enna and take the beacon with you Page 30 Apr 17 03 h ELTA USER S HANDBOOK C Beacon shutdown In the event of a false manoeuvre or untimely operation shutdown the beacon The beacon is shutdown by pressing the RESET TEST pushbutton on the remote control unit This control is not active during the self test sequence or if the ON ARMED switch is in ON position NOTE Stopping distress signal transmission by means of the remote control unit does not switch the beacon OFF It is restored in ARMED mode Acknowledgment of the control is displayed by 2 short blink on LED and buzzer CAUTION THE BEACON MUST BE SHUTDOWN BEFORE ANY MAINTENANCE OPERATIONS ARE PERFORMED THE BEACON MUST BE COMPLETELY SHUTDOWN BEFORE IT IS REMOVED AND IT S ARMED OFF ON TOGGLE SWITCH SHALL BE IN OFF POSITION D Beacon self test CAUTION THE SELF TEST SHALL BE PERFORMED WITHIN THE FIRST 5 MN OF ANY HOUR BECAUSE THE ELT IS SENDING 121 5 MHZ SIGNAL FOR 5 S DURING THIS PROCESS LIMITATION OF FALSE ALERT The ELT ADT 406 AP is designed to perform a self test from the remote control unit or as soon as the beacon is started up manually Actual test transmission on 121 5 MHz for 5 5 can be listen on any VHF receiver 1 Self test on the beacon CAUTION THIS SELF TEST PROCESS SHALL NOT BE INTERUPTED IF THIS PROCESS IS NOT COMPLETE FOR ANY REASON PERFORM A NEW COMPLETE SELF TEST Note in case of use in survival mode without exte
26. ficial 15 Hex selection C S identification ce i 7 CIS identification C S IDENTIFICATION simplified decoding e Batteries label This label indicates the batteries expiry date next battery servicing CONTAINS LITHIUM BATTERIES BATTERIES EXPIRY CONTIENT DES PILES LITHIUM PEREMPTION DES PILES fejmjalmjsjsfajsjoinjo LIMNO2 D LISOCL2 0 03 04 05 08 vo 10 11 12 13 14 Page 20 Apr 17 03 USER S HANDBOOK f Additional labels for CANADA There two additional labels related to CANADA application is related to Cospas Sarsat matters in CANADA is related to Battery part clarification for CANADA An example of these new labels are presented here under CANADIAN REQUIREMENTS 24 bit Address protocol is mandatory In case of ownership change ELT Cospas Sarsat coding must be updated Contact www elta fr CANADIAN REQUIREMENTS Battery replacement with P N 02N60052 Battery Servicing kit is mandatory Follow CMM 25 60 10 related tasks ELT ADT 406 AP aircraft components g Remote control unit The remote control unit integrated in the aircraft cockpit consists of a RESET TEST pushbutton an ELT ON indicator light 8 two position ON ARMED switch with safety cover flip guard The safety cover forces the switch to ARMED position This switch must always remain in this position except in the case of manual distress triggering
27. g tool Appendix B page 7 Feb 15 03 LOG BOOK ENCODING UPDATE FORM REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address _ A C REG MARKL C S 15 HEX SIMPLIFIED DEC A C MSN OR FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool REGISTRATION COUNTRY ELT SERIAL NUMBER PROTOCOL ELT S N OP DESIGNATOR sl A C 24 Bit Address __ A C REG C S 15 SIMPLIFIED DEC A C MSN OR A P FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE foret fosse MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding update sheet issued from the ELTA encoding tool Appendix B page 8 Feb 15 03 LOG BOOK MAINTENANCE TASKS FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE fatta MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool FINAL OPERATOR TYPE OF MAINTENANCE BATTERY SERVICINGL INSPECTION RF TASK DESCRIPTION NEXT BATTERY SERVICING ERE MM YYYY DATE MM DD YYYY REPAIR STATION
28. h ELTA USER S HANDBOOK USER S HANDBOOK INCLUDING INSTALLATION MANUAL AND LOG BOOK SERIAL NUMBER LABEL EMERGENCY LOCATOR TRANSMITTER MODEL ADT 406 AP PN 01N65910 IN THE COSPAS SARSAT SYSTEM Issued by ELTA F6614 14 Place Marcel Dassault 31702 BLAGNAC France www elta fr Documentation P N 03E61013 Rev Title Page Initial issue Feb 15 03 May 16 14 h b ELTR USER S HANDBOOK LIST OF UPDATES INSERTION INSERTION ISSUE ISSUE DATE BY DATE BY Feb 15 03 E LABRIFFE 1 B Apr 17 03 ELABRIFFE 2 May 16 14 ADOMPS Page 1 May 16 14 R Ga Nu ELTR USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK Page 2 BLANK h b ELTR USER S HANDBOOK LIST OF EFFECTIVE PAGES CHAPTER DATE CHAPTER DATE SECTION PANE SECTION TITLE PAGE May 16 14 Appendix 1 Feb 15 03 2 Feb 15 03 LISTE OF UPDATES 1 Apr 17 03 3 Feb 15 03 2 BLANK 4 Feb 15 03 5 Feb 15 03 LIST OF EFFECTIVE PAGE 3 Apr 17 03 Appendix B 4 BLANK 1 Feb 15 03 2 Feb 15 03 TABLE OF ILLUSTRATIONS 5 Feb 15 03 3 Feb 15 03 6 BLANK 4 Feb 15 03 5 Feb 15 03 LEADING PARTICULARS 7 Feb 15 03 6 Feb 15 03 8 BLANK 7 Feb 15 03 8 Feb 15 03 TABLE OF CONTENTS 9 Feb 15 03 9 Feb 15 03 10 BLANK 10 Feb 15 03 11 Feb 15 03 11 Feb 15 03 12 Feb 15 03 12 Feb 15 03 13 Feb 15 03 13 Feb 15 03 14 Apr 17 03 14 Feb 15 03 15 Apr 17 03 16 Apr 17 03 17 Apr 17
29. ipement avec ce marguage ITSO sik n est plus en conformit avec la r gle entation francaise ou les proc dures JAA concernant les autoris ti i 3150 The ITSO Authorisation Holder cannot identify an article wit this ITSO marking if he does not remain in compliance with the French regulation or with JAA proc dures for JTSO Authorisation 2 Sous r serve de satisfaire la condition pr c dente cette autorisation reste valide suf si elle a t restitu e suspendue ou retir e Subject to compliance with the foregoing condition this approval shall remain valid unless the approval has been surrendered suspended or revoked L ng nieur ar Chat de l mmement Vix du Burezu Motsum h lices quipemente B Ministre charge de l Aviation Civile fob PACEGALTIER Date d mission 29 avr 03 Date of issue Appendix A page 2 Feb 15 03 TSO C91a AND TSO C126 APPROVAL G e d AIRCRAFT CERTIFICATION STAFF U S Department elo American Embassy 27 Boulevard du Regent Koa Aviation f B 1000 Brussels Belgium June 12 2003 In reply refer to GE vk 06 12 03 0073 03 Mr Jacques Houget Direction Generale de l Aviation Civile 50 me Henry Farman F 75720 Paris Cedex 15 France Dear Mr Houget Based on the DGAC France certification and receipt of the required data we hereby accept ELTA TSO design approval to include the Emergency Locator Transmitters ELT listed below for manufacture at ELTA l
30. k up antenna length 375 mm deployed 3 General characteristics a External antenna Omnidirectionnal three frequency antenna 50Q access conform to COSPAS SARSAT and EUROCAE ED 62 specifications b Power supply High energy batteries 2 series connected packs activable for 5 years Autonomy 24 hours on 406 028 MHz and greater than 60 hours at 20 C on 121 5 amp 243 MHz Voltage 6 VDC capacity 10 5 ELTA type number 00E64191 lithium manganese dioxide solid cathode battery servicing kit available 02N60052 kit for one ELT 02N60053 kit for 10 ELT Page 16 Apr 17 03 h x ELTA USER S HANDBOOK c Radio electrical characteristics 1 406 MHz satellite transmitter Frequency 406 028 MHz transmitter power 5 W modulation L two phase transmission recurrence 50 s transmission duration 440 or 520 ms 2 Associated homing transmitter Frequency 121 5 MHz 243 Mhz or 121 5 MHz selectable 121 5 MHz transmitter power 140 mW 243 MHz transmitter power 140 mW modulation AM 3K20A3X type from 1600 Hz to 300 Hz up to four periods per second antenna gain gt 1 dBi d Environment characteristics Operating temperatures 20 C to 55 C storage temperatures 55 C to 85 C e Miscellaneous characteristics Automatic activation level in accordance with EUROCAE ED 62 internal G switch Activ
31. location that is sent via C S message 4 Ground reception stations The zone effectively covered or visibility zone is a circle with a radius of 2 500 km around the station These stations receive via the satellites and process in real time the messages from the beacons activated in their visibility zone and in batch mode the messages from the 406 MHz beacons activated outside that zone and memorized by the satellites Automatic processing of the 406 MHz digital messages allows the beacons to be located and the carrier mobile to be identified Page 13 Feb 15 03 h x ELTA USER S HANDBOOK 2 GENERAL DETAILS OF THE ELT ADT 406 AP A Purpose of the ELT ADT 406 AP Ref Fig 2 The ELT ADT 406 AP consists of a beacon that incorporates means of attachment The ELT ADT 406 AP is designed to transmit a digital distress signal to satellites that are part of the COSPAS SARSAT SYSTEM These satellites transmit the captured signal to the reception stations on the ground This signal is transmitted on the 406 028 MHz frequency and is used to precisely locate and identify the ELT ADT 406 AP It also transmits a 121 5 MHz and 243 MHz signal to facilitate the final approach of the distress scene homing It can be triggered manually or automatically by means of an acceleration sensor G switch in accordance to EUROCAE ED 62 standard This ELT meets the latest JAR OPS and ICAO recommendations Any encoding protocol defined b
32. ns called Local User Terminals LUT These ground stations determine the position of the emergency transmitters and then retransmit the position data to the designated Mission Control Centers MCC The MCCs in turn retransmit these data to the appropriate Rescue Coordination Centers RCC so that they can start the search and rescue operations J COSPAS SARSAT COSPAS Kosmicheskaya Sistyema Poiska Avariynych Sudov SARSAT Search and Rescue Satellite Aided Tracking Page 11 Feb 15 03 h b ELTR USER S HANDBOOK SATELLITES SARSAT COSPAS SAR FORCES 6MHz e x I gt io N Legend ELT Emergency Locator Transmitter EPIRB Emergency Position Indicating Radio Beacon PLB Personal Locator Beacon RCC Rescue Coordination Centers Mission Control Centers LUT Local User Terminals COSPAS SARSAT System Principle Figure 1 Page 12 Feb 15 03 h x ELTA USER S HANDBOOK C The distress frequencies There are several advantages to using the 406 MHz frequency Worldwide coverage locating is not only possible in real time within a radius of 2 500 km around the station but also in global mode outside this zone since the satellites memorize the messages on the 406 MHz frequency Location process uses Doppler effect Locating accuracy 2 km as opposed to 10 to 15 km in the 121 5 MHz or 243 MHz frequencies It should be noted however that the 406 MHz beacons also transmit 121 5
33. ntification module support 3 The ELT ADT 406 AP basic aircraft components consists of aremote control unit an external antenna Note this beacon can be used in survival mode without these elements B Detailed description Ref Fig 7 1 The ADT 406 AP beacon The ADT 406 AP beacon mainly consists of awhip antenna a power supply module an electronic assembly amechanical assembly afloat The front face of the electronic assy is equipped with the following components a REMOTE CONTROL electrical high density 15 pins female connector 10 for connecting up to the aircraft remote control panel or programming tools a BACK UP WHIP ANT TNC female connector 13 for connecting up the antenna an EXT ANT BNC female connector 9 for connecting up the external antenna an ARMED OFF ON lockable toggle switch 12 for activating the beacon aTX indicator light 11 indicating beacon activation real distress and self test Page 18 Feb 15 03 h x ELTA USER S HANDBOOK 2 The labels a ldentification label This label indicates beacon name manufacturer details the condition in which the beacon may be used warning approval number identification part number service bulletin serial number and conditions on the use of the beacon EMERGENCY LOCATOR TRANSMITTER BALISE DE DETRESSE ADT 406 AP COSPAS SARSAT 406 MHz 121 5 M
34. ocated at 14 Place Marcel Dassault BP 48 31702 Blagnac Cedex France Part Number Description P N 01N6591 Portable and Survival Txi Freg Automatic ELT Model ADT 406 P N 02N60051 Mounting Bracket Model ADT 406 AP P N 02N69004 Whip Antena Model ADT 406 AP Deviation The requested Automatic activation acceleration threshold Specified to 2 0 3 g 1 7 Eto2 3 g is increased by 0 3 g to obtain 2 3 0 3 g 2 0 to 2 6 g Appendix page 3 Feb 15 03 Any further deviations from the established design approval should be accomplished in accordance with FAR 21 609 The request for approval to deviate together with all pertinent data should be submitted to the Federal Aviation Administration FAA through the LBA and should contain information to show that the particular deviation is compensated for by factors or design features providing an equivalent level of safety The following statement must be furnished with each manufactured unit The conditions and tests required for TSO approval of this article are minimum performance standards It is the responsibility of those desiring to install this article either on or within a Specific type or class of aircraft to standards the article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the Administrator A letter of TSO design approval issued under FAR 21 617 is not transferable and is effective
35. rnal antenna the self test will indicate an antenna failure but the beacon will transmit normally on its emergency antenna Place the beacon s ARMED OFF ON toggle switch 12 in ON position After two short blinks and a delay of 3 s check that the indicator light 11 comes ON and the beacon s buzzer sounds during 6s After a brief blink the self test report is display 10s permanent illumination of the indicator light 11 for correct operation 10 s blinking condition of the indicator light 11 for failure detection Blinking rate indicates the failure source detection as follow 125 ms ON 125 ms OFF Frequency 4 Hz ELT Check Sum failure software problem 250 ms ON 250 ms OFF Frequency 2 Hz ELT power failure UHF and or VHF 500 ms ON 500 ms OFF Frequency 1 Hz Ext Antenna connection failure or signal identification missing Page 31 Apr 17 03 h ELTA USER S HANDBOOK Then the beacon enter in a waiting condition for 30 s rate 1 75s ON 0 25s OFF During this state return the switch 12 to ARMED position CAUTION OPERATOR SHALL SWITCH OFF OR ARMED THE ELT WITHIN 30 S AFTER SELF TEST REPORT TO AVOID REAL DISTRESS TRANSMISSION 2 Self test by means of the remote control unit The beacon s ARMED OFF ON toggle switch 12 must be in ARMED position The Remote Control ARMED ON must be in ARMED position Press the RESET TEST pushbutton until the two acknowlegment blink on LED Then after a delay
36. tallation of the beacon on the aircraft Ref Fig 4 In the case of use in automatic mode the beacon shall be installed in the rear of the aircraft in order to maximize the probability of ELT survival in case of crash However it can be installed in another position in survival mode The activation identification module DIRECTION OF FLIGHT must be parallel with the aircraft flight axis as indicated by the beacon s label The activation identification module direction and the A C forward aft directions must be respected to ensure correct acceleration sensor G switch operation See Fig 4 AIRCRAFT FLIGHT AXIS HORIZONTAL AXIS MAX 8 MAX sf MAX 8 MAX wi NOTE An angle of up to 8 from the aircraft flight axis could be allowed An angle of up to 3 from the aircraft horizontal axis could be allowed Tolerances on the Axis for Installation of the ELT ADT 406 AP Figure 4 Page 22 Feb 15 03 h x ELTA USER S HANDBOOK The beacon can be installed in any position normal upside down right side left side with respect with the G Switch activation direction stated on figure 4 The activation identification assy of the beacon can be installed in four positions Three alignment pins on the beacon board allow to set it in the required position A cap is installed in one of the four holes of the activation identification assy who is unused This cap shall be assigned upon the initial installation and will keep
37. this position in memory for further beacon replacement AIRCRAFT AIRCRAFT FRONT FRONT UNDERNEATH VIEW UNDERNEATH VIEW AIRCRAFT FRONT AIRCRAFT FRONT Unstowed objects must be not able to impact the beacon Attach the beacon to the fuselage of the aircraft by means of four M4 bolts Four 5 mm diameter holes at the corners of a 210 mm x 45 mm rectangle are drilled in the beacon Particular care must be taken with this attachment Standard industry means must be used to lock the screws Use flat washer in order to avoid paint damage The attachment points are similar to those of the ADT 406 AF AP beacon Page 23 Feb 15 03 h ELTA USER S HANDBOOK The figure 5 shows the drilling pattern dimensions and determine the required area to access to the beacon controls and connectors 210 8 27 18 8 0 74 2 21 LEAVE THIS AREA FREE TO PROVIDE ACCESS TO CONTROLS amp CONNECTIONS ELTA Recommendation 231 6 9 12 171028 60 2 36 a A E 152 5 98 33 13 Korpea 1 1 1 RA LOIN ae big ELT 2 KN I 4 8 a FRONT 5 g 1 40 1 46 O 1 5 5 o LEAVE THIS AREA FREE PROVIDE ACCESS TO CONTROLS amp CONNECTIONS 139 5 5 49 952 3 75 Optional for Other Beacon Retrofit Installation of the ELT
38. y COSPAS SARSAT can be used with ELT ADT 406 AP including country code assignation Activation identification Whip back up antenna Metalic stap Access to Access to external remote control unit or antenna BNC encoding tool Support ELT ADT 406 AP Presentation Figure 2 Page 14 Apr 17 03 h b ELTR USER S HANDBOOK 205 1 8 07 101 3 3 99 329 3 12 97 188 7 4 A N N tO 0 E pn PPAR 5 TE S 8 15 45 o SI 03P60296 gl N N tO LO Ne _ ELT ADT 406 AP Overall Dimensions Without optional protecting cover Figure 3 Page 15 Apr 17 03 h x ELTA USER S HANDBOOK B Characteristics Ref Fig 3 1 Approvals ADT 406 AP is COSPAS SARSAT approved TAC 131 dated July 2002 ADT 406 AP meets EUROCAE ED62 standard ADT 406 AP is JTSO 2 91 and JTSO 2C126 JTSO N F O 0112 dated April 29 2003 ADT 406 AP is TSO C91a and TSO C126 TSO letter dated June 12 2003 2 Physical characteristics a Beacon with support Height 101 3 mm Width 188 mm Length 329 3 mm Weight 2 1 kg or 2 15 kg with the option of a protecting cover b Beacon only Height 101 3 mm Width 188 mm Length 234 mm without back up antenna Weight 1 7 kg with back up antenna Bac
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