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USER’S HANDBOOK

Page 27

Oct 11/07

D. Remote control unit installation

The ELT ADT 406² AF / 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.

The following simplified diagram shows the wiring between the ELT ADT 406² AF / AP and its peripherals :

–  The Remote Control Panel (in cockpit) identified as "RCP",
–  the external antenna noted as "EA",
–  the back up antenna noted as "BA".

The EA is connected to the ELT ADT 406² AF / AP BNC female connector (5).

The BA is connected to the ELT ADT 406² AF / AP TNC female connector (1).

The RCP is connected to the ELT ADT 406² AF / AP high density 15 pins female Sub-D connector (3).
ELTA recommend to use P/N 28676 (or Type 8525-16R 14SN- or equivalent) to match RCP connector. See
drawing 05E66081 presented in Appendix A page 10 for details.

A three position guarded switch (2) controls the ELT ADT 406² AF / AP.

A red indicator (4) displays the ELT ADT 406² AF / AP state.

ADT 406² AF / AP Beacon Installation – Wiring Diagram Figure 7

4 wires
(not supplied)

ON / ARMED 1 E

ELT ACTIVATED 5 C

TEST / RESET 7 D

V BATT (HI) 13 F

RCP
CONNECTOR

ELT HD 15pt
CONNECTOR

02N64070 recommended

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Содержание 01N65900

Страница 1: ... 02 Title Page May 16 14 USER S HANDBOOK INCLUDING INSTALLATION MANUAL AND LOG BOOK EMERGENCY LOCATOR TRANSMITTER MODEL ADT406 AF AP PN 01N65900 IN THE COSPAS SARSAT SYSTEM Issued by ELTA F6614 14 Place Marcel Dassault 31702 BLAGNAC France www elta fr SERIAL NUMBER LABEL ...

Страница 2: ...USER S HANDBOOK PAGE INTENTIONALLY LEFT BLANK ...

Страница 3: ...INSERTION UPDATE No ISSUE DATE BY UPDATE No ISSUE DATE BY A B C D E F G INITIAL Update Update Update Update Update Update Jun 30 02 Apr 30 03 Jul 30 03 Jun 30 06 Oct 01 06 Oct 11 07 May 16 14 C CRESP E LABRIFFE E LABRIFFE E LABRIFFE E LABRIFFE C CRESP A DOMPS ...

Страница 4: ...USER S HANDBOOK Page 2 BLANK PAGE INTENTIONALLY LEFT BLANK ...

Страница 5: ...11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Appendix A Appendix B 1 2 3 4 5 6 7 8 9 10 11 12 13 14 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11 07 Oct 11...

Страница 6: ...USER S HANDBOOK Page 4 BLANK PAGE INTENTIONALLY LEFT BLANK ...

Страница 7: ...P Dimensions Basic Configuration 16 Figure 4 Tolerances on the Axis for Installation of the ELT ADT 406 AF AP 23 Figure 5 Automatic activation direction selection for ELT ADT 406 AF AP 24 Figure 6 Installation of the ELT ADT 406 AF AP Drilling Pattern Dimensions 25 Figure 7 ELT ADT 406 AF AP Installation Wiring Diagram 27 Figure 8 ELT ADT 406 AF AP Detailed Description 35 ...

Страница 8: ...USER S HANDBOOK Page 6 BLANK PAGE INTENTIONALLY LEFT BLANK ...

Страница 9: ...E TO THIS REGISTRATION CAUTION 3 THE BEACON MUST IMPERATIVELY BE PROGRAMMED WITH THE RELEVANT IDENTIFICATION AUTHORIZED BY THE LOCAL AIRWORTHINESS CAUTION 4 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 CAUTION 5 BEFORE INSTALLING OR USING THI...

Страница 10: ...USER S HANDBOOK Page 8 BLANK PAGE INTENTIONALLY LEFT BLANK ...

Страница 11: ...ral description 19 B Detailed description 19 4 INSTALLATION OF THE ELT ADT 406 AF AP 23 A General 23 B Installation of the beacon on the aircraft 23 C External antenna installation 26 D Remote control unit installation 27 E Installation and configuration of the beacon 28 5 UTILIZATION OF THE ELT ADT 406 AF AP 29 A Automatic activation 29 B Manual activation 29 C Beacon shutdown 30 D Beacon self te...

Страница 12: ...USER S HANDBOOK Page 10 BLANK PAGE INTENTIONALLY LEFT BLANK ...

Страница 13: ...lete 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...

Страница 14: ...end ELT Emergency Locator Transmitter EPIRB Emergency Position Indicating Radio Beacon PLB Personal Locator Beacon RCC Rescue Coordination Centers MCC Mission Control Centers LUT Local User Terminals COSPAS SARSAT System Principle Figure 1 ...

Страница 15: ... 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 po...

Страница 16: ...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 AF 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 manuall...

Страница 17: ...e memory and will not be lost upon module or battery removal The ADT 406 AF AP ELT can be operated in a non location protocol ELT when the transmitter is installed alone on board the A C Cospas Sarsat Identification message encoded as Short or in user location protocol ELT when the transmitter is installed with its optional dedicated Navigation Interface equipment that receive the A C location Lat...

Страница 18: ...USER S HANDBOOK Page 16 Oct 11 07 ELT ADT 406 AF AP Overall Dimensions Basic Configuration Other Back Up Antenna Configuration Are Available Figure 3 205 8 07 74 2 91 ...

Страница 19: ... letter dated November 24 2006 see Appendix A page 6 ADT 406 AF AP is IC approved Industrie Canada letter dated February 13 2007 see Appendix A page 8 2 Physical characteristics Height 74 mm Width 160 mm Length 234 mm without back up antenna Weight 1 6 kg maximum Back up antenna lenght 200 mm max 3 General characteristics a External antenna Omnidirectionnal three frequency antenna 50 access confor...

Страница 20: ...ttery self discharge rate e Miscellaneous characteristics Automatic activation level in accordance with EUROCAE ED 62 internal G switch see Appendix A page 13 Activation direction is selectable 4 possibe directions see Figure 5 color orange in conformity with the international distress code self test transmission of one 406 028 MHz burst modulated with inverted frame synchronization and 1s transmi...

Страница 21: ...F AP basic aircraft components consists of a remote control unit an external antenna B Detailed description Ref Fig 7 1 The ADT 406 AF AP beacon The ADT 406 AF AP beacon mainly consists of a power supply module an electronic assembly a mechanical assembly The front face of the electronic assy is equipped with the following components a REMOTE CONTROL electrical SUB D high density 15 pins female co...

Страница 22: ...ails 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 b How to use label This label gives indication on the electronic front face connectors and controls use versus mode of operation X JTSO 2C91a 2C126 ...

Страница 23: ...cation label This label indicates the axis according to which the ELT ADT 406 AF AP must be installed on the aircraft see paragraph 4 B for automatic activation G switch It is fixed to the activation identification module e Batteries label This label indicates the batteries expiry date next battery servicing Homing pwr xx dBm Homing power selection Official 15 Hex ...

Страница 24: ...in this position except in the case of manual distress triggering 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 cockp...

Страница 25: ...y systems If in doubt contact the aircraft manufacturer or its representative inspected by representative authority B Installation of the beacon on the aircraft Ref Fig 4 The beacon shall be installed in the rear of the aircraft in order to maximize the probability of ELT survival in case of crash The activation identification module DIRECTION OF FLIGHT must be parallel with the aircraft flight ax...

Страница 26: ...who is unused This cap shall be assigned upon the initial installation and will keep this position in memory for further beacon replacement Automatic activation direction selection for ELT ADT 406 AF AP Figure 5 Note With this ELT model the fixation holes are part of the case No additional bracket is required The presented four possible solutions of the Activation Identification module on the top ...

Страница 27: ...rect installation of the Activation Identification module it shall be attached to the A C by means of the metalic strap in order to keep on board A C the Cospas Sarsat identification information related to the installed ELT So these information will remain in the A C upon transmitter exchange for overhaul process as exemple Unstowed objects must be not able to impact the beacon Attach the beacon t...

Страница 28: ...pper 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 cl...

Страница 29: ... as BA The EA is connected to the ELT ADT 406 AF AP BNC female connector 5 The BA is connected to the ELT ADT 406 AF AP TNC female connector 1 The RCP is connected to the ELT ADT 406 AF AP high density 15 pins female Sub D connector 3 ELTA recommend to use P N 28676 or Type 8525 16R 14SN or equivalent to match RCP connector See drawing 05E66081 presented in Appendix A page 10 for details A three p...

Страница 30: ... ELT Switch the Remote Control ON ARMED lockable toggle switch to ARMED on remote control panel 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 CAUTION AS SOON AS THE BEA...

Страница 31: ...ter this delay the ELT will transmit actual distress signals on the three availables distress frequencies B Manual activation There are two cases in which a distress signal may be triggered manually the acceleration sensor G switch has not 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 ...

Страница 32: ...ET 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 blinks on beacon LED beacon buzzer and on Remote Control Uni...

Страница 33: ...dicator light 8 for correct operation 10 s blinking condition of the indicator light 8 for failure detection An easy way to detect the correct failure condition is simply to count the number blink during the 10 s self test report duration Blinking rate indicates the failure source detection as follow 10 blinks i e 500 ms ON 500 ms OFF Frequency 1 Hz Ext Antenna connection failure or identification...

Страница 34: ... operation 10 s blinking condition for failure detection An easy way to detect the correct failure condition is simply to count the number blink during the 10 s self test report duration Blinking rate indicates the failure source detection as follow 10 blinks i e 500 ms ON 500 ms OFF Frequency 1 Hz Ext Antenna connection failure or identification missing AIM can not be read 20 blinks i e 250 ms ON...

Страница 35: ...e performed when the order to do so is given or by the competent authorities A higher rate of self test is possible but will reduce the standard 5 years battery servicing interval 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 ...

Страница 36: ...ral overhaul when required and a complete verification on its test and programming bench at this occasion Refer to CMM 25 60 10 for detail of operation This information is summarized on the new label stuck on the ELT transmitter for CANADIAN applications presented here under only for Canada application D Batteries discarding The batteries must be discarded in compliance with the applicable regulat...

Страница 37: ...ACTIVATION IDENT ASSY 4 BACK FACE 5 MACHINED SECTION 6 EXT ANT BNC CONNECTOR FEMALE 7 REMOTE CONTROL CONNECTOR SUB D HD FEMALE 15 PINS 8 TX LED 9 ARMED OFF ON TOGGLE AND GUARDED SWITCH 10 BACK UP ANT TNC CONNECTOR FEMALE 11 METALIC STRAP ELT ADT 406 AF AP Detailed Description Figure 8 11 ...

Страница 38: ...Appendix A page 1 Oct 11 07 COSPAS SARSAT TYPE APPROVAL CERTIFICATE ...

Страница 39: ...Appendix A page 2 Oct 11 07 JTSO 2C91a AND JTSO 2C126 APPROVAL ...

Страница 40: ...Appendix A page 3 Oct 11 07 TSO C91a AND TSO C126 APPROVAL ...

Страница 41: ...Appendix A page 4 Oct 11 07 ...

Страница 42: ...Appendix A page 5 Oct 11 07 ...

Страница 43: ...Appendix A page 6 Oct 11 07 ...

Страница 44: ...Appendix A page 7 Oct 11 07 ...

Страница 45: ...Appendix A page 8 Oct 11 07 ...

Страница 46: ...Appendix A page 9 Oct 11 07 ...

Страница 47: ...Appendix A page 10 Oct 11 07 ...

Страница 48: ...Appendix A page 11 Oct 11 07 ...

Страница 49: ...Appendix A page 12 Oct 11 07 ...

Страница 50: ...Appendix A page 13 Oct 11 07 Crash Sensor Response Curve ...

Страница 51: ...Appendix A page 14 Oct 11 07 PAGE INTENTIONALLY LEFT BLANK ...

Страница 52: ...LOG BOOK Appendix B page 1 Oct 11 07 FACTORY SETTING NEXT BATTERY SERVICING MM YYYY ...

Страница 53: ...LOG BOOK Appendix B page 2 Oct 11 07 FACTORY SETTING ...

Страница 54: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 55: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 56: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 57: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 58: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 59: ...HONE 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 A C OP DESIGNATOR S N A C 24 Bit Address A C REG MARK TEST C S 15 HEX SIMPLIFIED DEC A C MSN A C OR A P TYPE FINAL OPERATOR CONTACT PHONE email ISSUED BY DATE MM DD YYYY SIGNATURE AND STAMP NOTE Attach the encoding...

Страница 60: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

Страница 61: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

Страница 62: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

Страница 63: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

Страница 64: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

Страница 65: ...ERVICING MM YYYY DATE 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 SERVICING INSPECTION REPAIR RF TEST TASK DESCRIPTION NEXT BATTERY SERVICING MM YYYY DATE MM DD YYYY REPAIR STATION SIGNATURE AND STAMP NOTE Attach the RF test sheet issued from the ELTA test tool ...

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