406 AF-Compact - Dallas Avionics
Contents
1. Check 121 5 MHz frequency using the aircraft tune receiver Refer to B 406 and 121 5 MHz transmission test page 302 B 6 year inspection Replacement of battery pack is mandatory every 6 years Refer to 2 Battery replacement requirements page 604 Testing of the following elements and parameters of the ELT is mandatory every 6 years together with the battery pack replacement Visual control of the housing and accessories Operation of the controls and crash sensor Measurement of 406 and 121 5 MHz output power and frequencies Verification of digital message coding 6 year inspection must be performed in the order listed below 1 Visual control of the housing and accessories Remove ELT from its mounting bracket Refer to 6 Removal page 207 Inspect the mounting bracket and the ELT Ensure the mounting bracket and the ELT are free of cracks or other obvious damage Inspect the connection Visually inspect all connector pins 2 Operation of the controls and crash sensor Refer to CMM 25 63 03 page block TESTING AND FAULT ISOLATION TASK 25 63 03 700 801 01 Beacon operating tests 3 Measurement of output powers frequencies and verification of digital message Refer to CMM 25 63 03 page block TESTING AND FAULT ISOLATION TASK 25 63 03 700 801 01 Beacon operating tests PAGE 602 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 4 Curr2. Figure 3 Installation controls and connectors Perform the first power up procedure see below 5 First power up Note Antenna and RCP must be connected Caution never switch to ARM or ON if neither antenna cable nor 50 ohm load is connected to the ELT 1 BNC connector risk of ELT damage Perform the following tests 1 ELT operational tests connect the outside antenna to J2 switch the ELT from OFF to ARM check that the Self Test result 15 OK one long flash 406 amp 121 5 MHz transmission tests optional Refer to B 406 and 121 5 MHz transmission test page 302 At the end of the first power up procedure switch the ELT to ARM The ELT is now in stand by mode and ready to be activated either automatically by G Switch sensor if a crash occurs manually by an optional Remote Control Panel when connected Note switching to ON directly on the ELT front panel will also activate the ELT PAGE 206 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 6 Removal Switch the ELT to OFF Disconnect the outside antenna from the BNC connector of the ELT If connected disconnect the DIN 12 Connector of Remote Control Panel 2 or 3 wire bundle from the DIN12 socket of the ELT Unfasten the self stripping strap Remove the transmitter from the bracket Figure 4 Removing the transmitter PAGE 207 SEP 16 2009 INSTALLAT
3. BNC connector for the antenna 4 2 Figure 201 Front Panel PAGE 101 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER The red light gives an indication on the working mode of the beacon after the self test aseries of short flashes indicate the self test failed one long flash indicates a correct self test in operating mode periodic flashes during 121 5 transmission long flash during 406 transmission A buzzer gives audio information on the beacon working continuous tone during self test 2 beeps per second during 121 5 transmission Silence during 406 transmission C Working mode information The ELT has 4 different modes Off Self test temporary mode Armed standby mode to enable automatic activation by the shock sensor or by an optional remote control panel On transmission Transmission is effective if the beacon is activated either manually on the ELT control panel automatically by the shock sensor or remotely by the ON switch of an optional remote control panel when connected 1 Off The ELT is off when the switch is in position OFF no part of the ELT is energized This mode must only be selected when the ELT is removed from the aircraft or when the aircraft is parked for a long period or for maintenance 2 Self Test The self test mode is a temporary mode max duration 15 sec in which the EL
4. error conditions were found A series of short flashes indicates the test has failed Remark The number of flashes gives an indication of the faulty parameter detected during the self test 341 LOW BATTERY VOLTAGE 342 LOW RF POWER 343 FAULTV VCO LOCKING FAULTV 344 NO IDENTIFICATION PROGRAMMED If self test fails contact the distributor as soon as possible Unless a waver is granted flight should be cancelled PAGE 301 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 Operational tests These tests must be performed by maintenance personnel when performing the first power up procedure or to check the transmitter Refer to B 406 and 121 5 MHz transmission test A ELT operational tests NOTE ELT operational tests only provide the aircraft operator with an indica tion that the ELT is transmitting however a positive result cannot be interpret ed as meaning that the ELT meets all operational parameters connect the outside antenna to J2 switch the ELT from OFF to ARM check that the Self Test result is OK one long flash B 406 and 121 5 MHz transmission test NOTE Transmissions tests only provide the aircraft operator with an indication that the ELT is transmitting however a positive result cannot be interpreted as meaning that the ELT meets all operational parameters 1 406 MHz This test must be carrie
5. Class COMPACT Class Il 20 C to 55 C COMPACT ER Class 1 40 C to 55 C 406 MHz TRANSMISSION Frequency 406 028 MHz 1 kHz Output power 5W 37 dBm 2 dB Modulation type 16K0G1D Biphase L encoding Transmission duration 440ms short message every 50 s Autonomy COMPACT over 48 hours 20 C COMPACT ER 24 Hours 40 C 121 5 MHz TRANSMISSION Frequencies 121 5 MHz 6 kHz Output power 100 to 400 mW 20dBm to 26 dBm Modulation type 3K20A3X Modulation rate 85 96 Frequency of modulation signal 1420 Hz to 490 Hz with decreasing sweep Autonomy COMPACT over 48 hours 20 C COMPACT ER over 48 hours 40 C CONTROLS ARM OFF ON switch DIN12 socket for RCP and pin programming option Bright red visual indicator Buzzer BNC antenna connector G SWITCH SENSOR Mechanical G switch sensor compliant with EUROCAE ED amp 62 specifications BATTERY KIT BAT200 P N 51840510 01 LiMnO two element battery for transmitter power supply Replacement 6 years after date of manufacture HOUSING Material Polycarbonate Color Yellow color compounded Transmitter dimensions 131 x 86 x 75 4 mm 5 157 x 3 385 x 2 968 inches Overall dimensions with mounting bracket max 140 x 98 x 86 4 mm 5 512 x 3 858 x 3 4 inches Weight including batteries typical 850 gr 1 874 Ib max 875 gr 1 929 Ib Tightness O ring ENVIRONMENTAL CONDITIONS RTCA DO 160E EUROCAE Section 4 to 26
6. ELT should remain in the ARM position except when the aircraft is parked for a long period or for maintenance 4 On This mode is selected manually by switching the ELT to ON by switching an optional Remote Control Panel switch to ON provided that the ELT switch is in the ARM position automatically when a crash occurs provided that the ELT switch is in the ARM position When this mode is selected the ELT starts transmitting after 50 seconds on 406 MHz one 406 MHz burst every 50 seconds on 121 5 MHz continous transmission between each 406 MHz burst The red visual indicator on the ELT and on an optional remote control panel when connected flashes and the buzzer operates Red visual indicator 1 short flash during ELT transmission on 121 5 MHz every 0 7 PAGE 103 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER seconds 1 long flash during ELT transmission on 406 MHz every 50 seconds Buzzer 1 5 Hz pulse signal recurrence 0 7 s during ELT transmission on 121 5 MHz In case of accidental activation the ELT can be reset either by switching it to OFF or by switching to RESET on an optional Remote Control Panel when connected The number of 406 MHz bursts transmitted is recorded This information is available when the ELT is connected to a programming and test equipment PR600 D Autonomy The ene
7. the 6 digits of the CSN number If the pin programming option is selected by the owner the following equipment are required a Programming Dongle on each aircraft e Maintenance Dongle on each ELT spare Figure 1 Maintenance Dongle PAGE 203 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 3 ELT transmitter installation procedure NOTE Intial installation bracket installation and first wiring is described in Initial installation manual DOC07089 also supplied with the transmitter 1 Mount the transmitter on the bracket Flight direction arrow pointed towards the front of the aircraft Refer to 2 KANNAD 406 AF COMPACT axis of installation page 502 Slide the self stripping strap through the buckle Ensure the buckle is correctly positioned indifferently on right or left side of ELT regarding the horizontal center line of ELT as shown Detail A PAGE 204 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 3 Fasten the self stripping strap tightly Figure 2 Installing the transmitter on the bracket PAGE 205 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 4 ELT transmitter Connection 1 Connect the cable of the outside antenna to the BNC connector of the front panel 2 Set the 3 position switch of the front panel to ARM
8. 406 MHz COSPAS SARSAT frequency for precise pinpointing and identification of the aircraft in distress 121 5 MHz used for homing in the final stages of the rescue operations The KANNAD 406 AF COMPACT and 406 AF COMPACT ER are certified as Automatic Fixed AF ELTs with the approved outside antennas The housing of KANNAD 406 AF COMPACT and 406 AF COMPACT ER transmitters are made of moulded plastic with excellent mechanical resistance The ELT housing is designed with no sharp edges Figure 3 ELT Transmitter PAGE 5 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER B Bracket The bracket installed near the tail is designed to fix the ELT with a Velcro strap This enables quick removal of the ELT for maintenance or exchange Velcro strap Bracket Figure 4 ELT Transmitter with Mounting Bracket The transmitter may be installed on its standard mounting bracket P N 51840502 01 or on an Universal Mounting Bracket P N S1840502 02 to re use existing drilling for retrofit Refer to DOC07089 Initial Installation Manual for drilling masks and outline dimensions of these brackets C Outside antenna Only approved antennas may be installed Refer to Section 6 Compatibility list page 108 Connection to the ELT will be carried out with a 50 Ohm coaxial cable RG58 for example ended with a male BNC connector IMPORTANT NOTICE KANNAD recommends a cable with radio e
9. C1X ED62 A ED62 SYLMC UGJEVXXXXZXXXIZCI ED62 B XXXXX XXX ED62 QUALIFICATIONS ETSO 2C91a amp ETSO 2C126 TSO C126 FOR USE OUTSIDE OF THE USA OR EASA RULES CONTACT YOUR LOCAL CIVIL AVIATION AUTHORITY 2 Equipment limitations None PAGE 106 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 3 Activation A Standby mode for automatic activation In order to be automatically activated by the crash sensor the ELT must be in standby mode This mode is mandatory during the flight We recommend to switch off the ELT only when removed from the aircraft or when the aircraft is parked for a long period or for a maintenance operation Check that the antenna is correctly connected Switch to ARM To operate the ELT with an optional Remote Control Panel ensure that The ELT switch is the ARM position B Manual activation Check that the antenna is correctly connected Switch to either on the ELT or on an optional Remote Control Panel when connected The ELT starts with the self test sequence then after 50 sec transmits On 406 MHz one 406 MHz burst every 50 seconds 121 5 MHz continous transmission between each 406 MHz burst During transmission the buzzer operates and the red visual indicator flashes 4 Off It is possible to stop the ELT in case of unintentional activation e Switch to OFF Regulations sta
10. DOC08038D Ref 0145599D lt 2 INSTALLATION MANUAL OPERATION MANUAL ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER o o c 6 E G o l gt o L I LU Revision 03 uodn gVNNVM oi AJ9IBIDOLLLII eq JJEUS eui QVNNVM Aq ay Aq pesn jou JJBUS y Jey pue 10 1uesuoo ssasdxa y JNOUJIM POSOJJSIP aq 1245 peurejuoo y JOU JJOSJI eu 121 sse1dxo y uo SI JUBWINDOP 9U Bguepyuoo pue pue Jo aui SI 5141 Date of rev MAY 05 2010 First issue JUN 10 2008 Users kindly requested to notify KANNAD of any discrepancy omission or error found in this manual Please report to our customer support E mail support sar kannad com Tel 33 0 2 97 02 49 00 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER RECORD OF REVISIONS REVISION DATE INSERTION DATE JUN 10 2008 JUN 10 2008 MAR 02 2009 MAR 02 2009 SEP 16 2009 SEP 16 2009 MAY 05 2010 MAY 05 2010 ROR PAGE 1 MAY 05 2010 INSTALLATION MANUAL OPERATION MANUAL KAN
11. ION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER E Electrical interfaces J1 DIN 12 socket J1 is dedicated for connection to an optional Remote Control Panel to a Programming or Maintenance Dongles or to a programming equipment PR600 IMPORTANT Shielded cables are recommended The required wires are AWG24 J1 PIN Signal Name Destination Direction J1 A JRCP TEST RESET J1 B DONGLE RX SMM PGM Viewed from J1 C DONGLE CS SMM Front Face J1 D DONGLE SK SMM J1 E DONGLE TX SMM PGM 9 Jt F DONGLE 2 _ 5 4 J1 G COMMON RCP J1 H RCP BUZZER Ji J RCPLED J1 K RCP RCP J1 L DONGLE GND SMM PGM J1 M COMMON RCP Table 1 J1 connector pin out J2 BNC female connector J2 is used to connect the outside antenna through a 50 coaxial cable IMPORTANT NOTICE The length of the coaxial cable should not exceed 2 7 meters 9 ft for a standard RG58 or equivalent coaxial cable If the cable length exceeds 2 7 meters a low loss cable of attenuation less than 1 dB 2400 MHz must be used See Important notice Section C Outside antenna page 6 PAGE 105 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER F Transmitter Technical Specifications TYPE Two frequency ELT 121 5 406 028 MHz Automatic fixed COSPAS SARSAT
12. ION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER PAGE INTENTIONALLY LEFT BLANK PAGE 208 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 1 Self test A Periodicity It is recommended by the manufacturer to test the ELT to detect any possible failure Operational check must be performed regularly by a pilot or maintenance personnel from the cockpit Remote Control Panel It is recommended to perform a self test once a month but it should not be done more than once a week Each self test consumes energy from the battery Should self tests be carried out more often than the maximum allowed the battery life time might be shorter than specified B Self test procedure Check that the antenna is correctly connected Do not perform self test without antenna connected Tune aircraft radio to 121 5 MHz and ensure you can hear it Switch from position OFF to position ARM or press RESET amp TEST on the Remote Control Panel ensure that the ELT switch is in position ARM Listen for the buzzer it operates during the whole Self test procedure Close to the end of self test a short 3 4 sweeps 121 5 transmission is made confirm this on the aircraft radio After a few seconds the test result is displayed with the red visual indicator and the buzzer will sound One long flash indicates that the system is operational and that
13. MS 1 ELT Outline Dimensions inches in brackets 140 5 512 o G 9 o c Co o 86 4 3 40 Arm Off On 98 3 858 PAGE 501 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 KANNAD 406 AF COMPACT axis of installation YAW Axis Front face o connectors Roll Axis Direction of Flight Arrow x gt 5 2 8 z bi 8 5 9 o 2 Pi 3 4 HEE 8 lt Di PAGE 502 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL SERVICING 1 Maintenance Schedule Battery replacement carried out by an accredited PART 145 or FAR 145 or equivalent maintenance station Periodic inspection depending if the ELT is opened or not PART 145 or FAR 145 or equivalent may be required Refer to local regulations IMPORTANT Inspections must be recorded on the ELT LOG SHEET ref DIM08013 supplied with the ELT fields Periodic Inspection log page 2 2 A Periodic inspection Note if required by the relevant Civil Aviation Authority Some Civil Aviation Authorities may require the ELT be tested periodically In this case it is recommended to check the following parameters Proper installation Operation of the controls and crash sensor Transmitted signals Battery corrosion Note Due to the technology
14. NAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER RECORD OF REVISIONS PAGE INTENTIONALLY LEFT BLANK ROR PAGE 2 MAY 05 2010 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER LIST OF EFFECTIVE PAGES SUBJECT PAGE DATE Title Page MAY 05 2010 Record of Revisions MAY 05 2010 MAY 05 2010 List of Effective Pages MAY 05 2010 MAY 05 2010 Table of Contents SEP 16 2009 SEP 16 2009 SEP 16 2009 SEP 16 2009 Introduction SEP 16 2009 SEP 16 2009 System Overview SEP 16 2009 SEP 16 2009 SEP 16 2009 SEP 16 2009 SEP 16 2009 SEP 16 2009 System Functional Description and Operation SEP 16 2009 SEP 16 2009 LEP PAGE 1 MAY 05 2010 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER LIST OF EFFECTIVE PAGES SUBJECT PAGE DATE 103 SEP 16 2009 104 SEP 16 2009 105 SEP 16 2009 106 SEP 16 2009 107 SEP 16 2009 108 MAY 05 2010 Installation Removal 201 SEP 16 2009 202 SEP 16 2009 203 SEP 16 2009 204 SEP 16 2009 205 SEP 16 2009 206 SEP 16 2009 301 SEP 16 2009 302 SEP 16 2009 303 SEP 16 2009 304 SEP 16 2009 Troubleshooting 401 SEP 16 2009 402 SEP 16 2009 Schematics and Diagrams 501 SEP 16 2009 502 SEP 16 2009 Servicing 601 SEP 16 2009 LEP PAGE 2 MAY 05 2010 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER LIST
15. OF EFFECTIVE PAGES PAGE DATE 602 SEP 16 2009 603 SEP 16 2009 604 SEP 16 2009 SUBJECT LEP PAGE 3 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER LIST OF EFFECTIVE PAGES PAGE INTENTIONALLY LEFT BLANK LEP PAGE 4 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER TABLE OF CONTENTS INTRODUCTION WARRANTY Exclusion SYSTEM OVERVIEW COSPAS SARSAT System Description World coverage with the COSPAS SARSAT system Operation Environmental improvements of ELTs KANNAD 406 ELT System Presentation LINE REPLACEABLE UNITS Transmitter Bracket Outside antenna SYSTEM FUNCTIONAL DESCRIPTION AND OPERATION Transmitter Functional Description Transmission Controls amp Connectors Working mode information Self Test Autonomy KANNAD 406 AF COMPACT P N 51840501 01 KANNAD 406 AF COMPACT ER P N S1840501 04 Electrical interfaces Transmitter Technical Specifications Equipment limitations Activation Standby mode for automatic activation Manual activation Self Test Compatibility list Mounting brackets Remote control panels RCP DIN 12 connector or programming dongles Outside antennas INSTALLATION REMOVAL Registration General TOC PAGE 1 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER TABLE OF CONTENTS Registratio
16. T checks the main characteristics of the transmitter Battery voltage Programming and enables digital communication with programming and test equipment This mode is selected when switching from OFF to ARM when switching to RESET TEST on an optional Remote Control Panel provided that the switch of the ELT is in position ARM when switching to ON prior to transmission The buzzer operates during the self test procedure PAGE 102 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER After about 10 seconds the test result is displayed on the visual indicator as follows One long flash indicates valid test Aseries of short flashes indicates false test result The number of flashes indicates the type of failure 3 1 LOW BATTERY VOLTAGE 3 2 LOW TRANSMISSION POWER e 3 3 FAULTY VCO LOCKING FAULTY FREQUENCY e 3 4 NO IDENTIFICATION PROGRAMMED It is recommended to test the ELT regularly in order to detect any possible failure Refer to A Periodicity page 301 The number of self tests carried out is recorded This information is available when the ELT is connected to a programming and test equipment PR600 3 Armed In order to enable activation by the G Switch or with an optional Remote Control Panel the ELT must be in standby mode with the switch in the ARM position This mode is mandatory during flight The
17. TALLATION REMOVAL 1 Registration A General The ELT must be registered prior to installation onboard When a 406 MHz ELT is installed in an aircraft it is imperative that the aircraft owner register the ELT Each 406 MHz ELT contains a unique identification code that is transmitted to the satellite This helps the Rescue Coordination Center RCC determine whether an emergency has actually occurred The unique identification permits accessing a data base The registration card available from the local registration authority must be completed and returned to this authority The Programming Datasheet DIM00300 must be completed and returned to your distributor Any change of ownership shall also be declared and registered with the local registration authority and with the distributor B Registration in USA Mail or Fax your registration form to NOAA SARSAT NSOF E SP3 4231 Suitland Road Suitland MD 20746 or Save Time Register your beacon online at www beaconregistration noaa gov All online registrations will be entered into the National 406 MHz Beacon Registration Database on the same day of entry Registration forms received via postal mail will be entered within 2 business days of receipt For online registrations a confirmation letter with your completed registration information form will be sent immediately via e mail or fax if provided Confirmation letters sent via postal mail should arrive within two weeks On
18. The main evolution consists in the extension to 40 C of temperature range The capability to connect either a 3 wire or 2 wire RCP is also applied to the KANNAD 406 AF COMPACT and 406 AF COMPACT ER The instructions in this manual provide the information necessary for the installation and the operation of KANNAD 406 AF COMPACT and 406 AF COMPACT ER ELTs Servicing instructions of ELT are normally performed by shop personnel For detailed instructions and identification parts list refer to CMM 25 63 03 For the initial installation please refer to Initial Installation Manual supplied with KANNAD 406 AF COMPACT and 406 AF COMPACT ER ELTs FOR REGULATORY REQUIREMENTS PLEASE CONSULT YOUR NATIONAL AVIATION AUTHORITY PAGE INTRO 1 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER WARRANTY 1 Scope The equipment is warranted against all material or manufacturing defect for a period of two years from the date of installation on the aircraft or thirty months for the date of shipment from KANNAD S A S Z I des Chemins BP23 56520 Guidel France whichever occur first Work carried out under the warranty shall not have the effect of extending the warranty period In respect of this warranty after a defect has been noted by our services the sole obligation incumbent upon us shall be the repair of the equipment or the element identified as being defective by our se
19. ce your registration confirmation is received please review all information Any changes or updates to your registration information can be done via the internet fax e mail or postal mail If you do not receive your registration confirmation from NOAA on the same day you submit it over the internet or within two weeks if you submit it by postal mail please call NOAA toll free at 1 888 212 SAVE 7283 or 301 817 4515 for assistance After initial registration or re registration you will receive a NOAA Proof of PAGE 201 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER Registration Decal by postal mail This decal is to be affixed to the beacon and should be placed in such a way that it is clearly visible If for some reason you do not receive the registration decal within two weeks please call NOAA toll free at 1 888 212 SAVE 7283 or 301 817 4515 Failure to register re register as required every two years or to notify NOAA of any changes to the status of your 406 MHz beacon could result in penalties and or fines being issued under Federal Law The owner or user of the beacon is required to notify NOAA of any changes to the registration information at any time By submitting this registration the owner operator or legally authorized agent declares under penalty of law that all information in the registration information is true accurate and complete Providing informat
20. d out with a COSPAS SARSAT decoder Perform self test switch ELT from OFF to ARM Check with the COSPAS SARSAT decoder that except for the 5th and the 6th digits the decoded message is identical to the programmed message NOTE The message transmitted during self test sequence always begins with FF FE 00 whereas a programmed message begins with FF FE 2F Example of message programmed in ELT FF FE 2F 53 C3 24 97 38 A6 OF 00 F5 20 Example of same message decoded by Cospas Sarsat Decoder FF FE DO 53 C3 24 97 38 6 OF DO F5 20 PAGE 302 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 121 5 MHz This check shall only be conducted during the first five minutes of any UTC co ordinated universal time hour and restricted in duration to not more than five seconds Be sure to notify any nearby control tower of your intentions This test must be carried out with a VHF receiver Aircraft VHF receiver may be used Tune VHF receiver to 121 5 MHz e Start transmission Switch ELT to ON Only 2 sweep tones are heard after 5 seconds then the 121 5 MHz stops Stop transmission Switch to OFF continue to listen to 121 5 MHz for a few seconds to ensure that the ELT does not continue to transmit after the test is terminated IMPORTANT If the ELT operates for approximately 50 seconds a 406 MHz signal is transmitted and is considered valid by t
21. d to match the various applications of the COSPAS SARSAT system EPIRB Emergency Position Indicating Radio Beacon for maritime applications ELT Emergency Locator Transmitter for aeronautical applications PLB Personal Locator Beacon for land expeditions Figure 1 COSPAS SARSAT System PAGE 1 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER B World coverage with the COSPAS SARSAT system The major improvement is the use of the COSPAS SARSAT system for processing aeronautical emergencies The 406 MHz transmission carries digital data which enable the identification of the aircraft in distress and facilitate SAR operation type of the aircraft number of passengers type of emergency The 406 MHz message is transmitted to the COSPAS SARSAT satellites This message is downloaded to one of the 64 ground stations 44 LEOLUTs and 20 GEOLUTS The aircraft is located by Doppler effect by the LEO satellites with a precision better than 2 NM 4 km at any point of the earth The 121 5 MHz frequency is no more processed by COSPAS SARSAT system but is still used by SAR services for homing in the final stage of rescue operations C Operation In the event of a crash the ELT activates automatically and transmits a sweep tone on 121 5 MHz and the 406 MHz signal In a crash a G Switch shock detector turns the ELT ON when the ELT is subjected to an important cha
22. e at http www nss gc ca site cospas sarsat INTRO e asp PAGE 202 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 Programming A Pin programming option The KANNAD 406 AF COMPACT and 406 AF COMPACT ER offer pin programming capabilities to facilitate maintenance operations especially in the case of removals and or replacement A special DIN 12 connector with a Serial Memory Module called Programming Dongle is connected to the ELT when installed onboard This Programming Dongle contains the identification information of the aircraft and remains onboard the aircraft When an unprogrammed ELT is installed and connected to this Programming Dongle and the ELT is switched to ARM it automatically updates its own memory with the identification data contained in the Programming Dongle memory When the ELT is removed from the aircraft it keeps its identification data For maintenance purposes it is possible to delete the identification information of the ELT by connecting a Maintenance Dongle to the ELT Any accidental transmission with this maintenance dongle will not involve SAR operation as the identification code transmitted is recognised by COSPAS SARSAT as not onboard When a maintenance dongle is connected Country code is 227 France Protocol is Test Identification number is SI 5 digits the last 5 digits of CSN number or K 6 digits
23. ent draw measurement in ARM and ON positions optional This test is required by Canadian Regulation according to CAR571 Appendix G c 3 d Refer to CMM 25 63 03 page block TESTING AND FAULT ISOLATION TASK 25 63 03 700 801 01 Beacon operating tests 5 Battery pack replacement CAUTION USE ONLY ORIGINAL AND APPROVED BATTERY PACK see 2 Battery replacement requirements Refer to CMM 25 63 03 page block DISASSEMBLY TASK 25 63 03 000 801 A01 and page block ASSEMBLY TASK 25 63 03 400 802 A01 6 Check of 121 5 MHz frequency Re install the ELT Refer to 3 ELT transmitter installation procedure page 204 Check 121 5 MHz frequency using the aircraft tune receiver Refer to B 406 and 121 5 MHz transmission test page 302 PAGE 603 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 Battery replacement requirements Battery replacement is mandatory after more than 1 hour of real transmission cumulated duration before or on the battery expiration date after use in an emergency after an inadvertant activation of unknown duration Only original and approved battery pack included in battery KIT BAT200 P N S1840510 01 supplied by KANNAD can be installed SAFT FRIWO Lithium Manganese Dioxide 2 x M20 D type cells PLEASE CONTACT YOUR LOCAL DISTRIBUTOR KANNAD refuse all responsibility and invalidate all warranty should other packs be installed Batter
24. he satellite system Switch ELT to ARM PAGE 303 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER PAGE INTENTIONALLY LEFT BLANK PAGE 304 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER TROUBLESHOOTING 1 General Procedure for fault isolation onboard uses the indicator light red visual indicator of the ELT s front panel This indicator light is activated by a self test capability within the ELT 2 Faults on Self test A Visual Indicator When the self test is carried out the number of flashes gives an indication of the faulty parameter detected during the self test 1 3 1 flashes Low battery voltage Replace battery refer to CMM 25 63 03 for tests and repair 2 3 2 flashes Low RF power Check 406 MHz power refer to CMM 25 63 03 for tests and repair 3 343 flashes Faulty VCO locking faulty frequency Check frequencies refer to CMM 25 63 03 for tests and repair 4 3 4 flashes No identification programmed Check programming refer to CMM 25 63 03 for tests and repair PAGE 401 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER PAGE INTENTIONALLY LEFT BLANK PAGE 402 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER SCHEMATICS amp DIAGRA
25. ion that is knowingly false or inaccurate may be punishable under Federal Statutes Solicitation of this information is authorized by Title 47 Parts 80 87 and 95 of the U S Code of Federal Regulations CFR Additional registration forms can be found on the NOAA SARSAT website at www sarsat noaa gov or at www beaconregistration noaa gov C Registration in Canada Beacon information is held in the Canadian Beacon Registry maintained by the National Search and Rescue Secretariat for use in search and rescue operations Online access to the Registry is available for all beacon owners to register new beacons or to update their beacon information You can add or update your beacon information by accessing the registry directly sending ina completed registration form or by talking to one of our beacon registry representatives You can access the registry online www canadianbeaconregistry com by email CBR Sarnet dnd ca by fax 1 613 996 3746 by telephone 1 800 727 9414 or 1 613 996 1616 The registration information must be updated when the aircraft ownership changes as per the Canadian Airworthiness Notice AN 029 refer to following link http www nss gc ca site Emergency Beacons canadian beacon registry e asp This information must be recorded on the ELT LOG SHEET ref DIM08013 supplied with the ELT fields Programming Log Additional information and registration forms can be found on the Canadian NSS websit
26. lectric properties similar or better to those of a RG58 cable The maximum permitted attenuation in the coaxial is 1 db at 400 MHz Note the 50 Ohm coaxial and the male BNC connector are not supplied PAGE 6 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL SYSTEM FUNCTIONAL DESCRIPTION AND OPERATION 1 Transmitter Functional Description A Transmission The transmitter can be activated either automatically when the crash occurs thanks to a shock sensor or manually thanks to a switch on the transmitter itself or on a RCP The transmitter is designed to transmit on two frequencies 121 5 and 406 MHz The 121 5 Mhz is mainly used for homing in the final stages of the rescue operations The 406 MHz frequency is used by the COSPAS SARSAT satellites for precise pinpointing and identification of the aircraft in distress Once activated the transmitter operates continuously on 121 5 MHz with an output power of 100 mW The modulation is an audio frequency sweeping downwards from 1420 Hz to 490 Hz with a repetition rate of 3 Hz During operations a digital message is transmitted on 406 028 MHz every 50 seconds The output power on 406 MHz is 5 W typical B Controls amp Connectors The following controls are to be found on the ELT front panel from left to right 3 position switch ARM OFF ON Visual indicator red DIN 12 socket for connection to an optional Remote Control Panel a programming dongle or a programming equipment
27. n in USA Registration in Canada Programming Pin programming option ELT transmitter installation procedure ELT transmitter Connection First power up Removal Self test Periodicity Self test procedure Operational tests ELT operational tests 406 and 121 5 MHz transmission test 406 MHz 121 5 MHz TROUBLESHOOTING General Faults on Self test Visual Indicator 3 1 flashes 3 2 flashes 3 3 flashes 3 4 flashes SCHEMATICS amp DIAGRAMS ELT Outline Dimensions KANNAD 406 AF COMPACT axis of installation SERVICING Maintenance Schedule Periodic inspection Proper installation Operation of the control crash sensor Transmitted signals Batteries corrosion Check of 121 5 MHz frequency 6 year inspection Visual control of the housing and accessories Operation of the controls and crash sensor Measurement of output powers frequencies and verification of digital message 602 Current draw measurement in ARM and ON positions optional Battery pack replacement Check of 121 5 MHz frequency Battery replacement requirements TOC PAGE 2 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER INTRODUCTION The KANNAD 406 AF COMPACT has been designed to satisfy the requirements of general aviation pilots built on the long experience of KANNAD ELTs in 406 MHz technology in aviation maritime and land distress beacons The KANNAD 406 AF COMPACT ER ELT is an evolution of KANNAD 406 AF COMPACT ELT
28. nge of velocity or deceleration Activation may also be accomplish by means of a Remote Control Panel RCP from the cockpit or directly from a switch of the ELT s front panel D Environmental improvements of ELTs The certification of an ELT includes a range of severe mechanical tests resistance to flame impact and crush tests resistance to 100 G and 500 G shocks watertightness anti deflagration extreme temperatures PAGE 2 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 2 KANNAD 406 ELT System Presentation KANNAD 406 AF COMPACT and 406 AF COMPACT ER belong to the AF type of ELTs which are permanently attached to an aircraft The KANNAD 406 AF COMPACT is designed to be installed on fixed wing aircraft or helicopters The KANNAD 406 AF COMPACT ELT system Refer to Section Figure 2 ELT system description page 4 is composed of 1 the ELT transmitter P N 51840501 01 for KANNAD 406 AF COMPACT or P N S1840501 04 for KANNAD 406 AF COMPACT ER a mounting bracket P N 51840502 01 or 51840502 02 an outside whip or rod antenna A remote control panel a DIN 12 connector or programming dongle when the optional RCP is connected Note 1 The RCP is optional only if the commands and controls of the ELT are reachable and visible from the pilot seated position RTCA DO 204A Equipment control and indicator installed for in flight use shall be
29. readily accessible from the cockpit crew position The cockpit crew shall have an unobstructed view of visual indicator when in the normal seated position For details of approved part number of KANNAD 406 AF COMPACT system Refer to Section 6 Compatibility list page 108 The transmitter and bracket are installed in the aircraft near the tail The outside antenna is mounted on the fuselage near the tail The remote control panel is installed in the cockpit and connected to the ELT with a DIN 12 connector or a programming dongle and a 2 or 3 wire bundle not supplied IMPORTANT Only transmitters P N 51840501 01 at amendment M higher and transmitters P N S1840501 04 are compatible with 2 wire RCP such as an RC102 CAUTION If a transmitter P N 51840501 01 at amendment M or higher should be replaced by a transmitter P N 51840501 01 at amendement L or lower check that it is not connected to a 2 wire RCP such as an RC102 PAGE 3 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER Figure 2 ELT system description Antennas not to scale Coaxial cable BNC Connector PAGE 4 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 3 LINE REPLACEABLE UNITS A Transmitter The KANNAD 406 AF COMPACT and 406 AF COMPACT ER are ELTs designed to be installed onboard aircraft to transmit a distress signal on frequencies
30. rgy is provided by a battery pack composed of a LiMnOs two element battery See pages 106 amp 604 for Kit battery reference Lithium cells lithium batteries and equipment containing such batteries are subjected to regulations and classified under class 9 as from 1st of January 2003 The transmitter battery expiry date is fixed at 6 years after manufacturing If no activation of the ELT occurs during the battery lifetime it shall be replaced 6 years after date of manufacture See note below NOTE The useful life time of batteries is twelve 12 years To be in compliance with FAR regulations they have to be replaced six 6 years after date of manufacture when 50 percent of their useful life has expired 1 KANNAD 406 AF COMPACT P N 51840501 01 The duration of the 121 5 transmissions is over 48 hours at 20 C Unlike other ELTs the 406 MHz transmission of KANNAD 406 AF COMPACT is not stopped after 24 hours and 406 MHz transmission is continuing beyond 48 hours 2 KANNAD 406 AF COMPACT ER P N 51840501 04 The duration of the 121 5 transmissions is over 48 hours at 40 C As it is therefore preferable to keep the battery power for 121 5 MHz homing frequency transmission for the rescue operations in compliance with COSPAS SARSAT specifications the 406 MHz transmission is deliberately stopped after 24 hours to extend the 121 5 MHz transmission for as long as possible PAGE 104 SEP 16 2009 INSTALLATION MANUAL OPERAT
31. rvices or possibly its replacement free of charge to the exclusion of all compensation or damages This warranty covers the cost of parts and labour in our factories The cost of transportation of the equipment replaced or repaired are the purchaser s exclusive responsibility The risks shall be borne by the purchaser 2 Exclusion Defects and deterioration caused by natural wear of the product or by external accident poor maintenance abnormal conditions of use etc or by modification of the equipment and tools not recommended nor specified by our company are excluded from the warranty Also the warranty shall not cover visible defects which the purchaser wouldn t have formally notified KANNAD within 48 hours of receipt of the equipment PAGE INTRO 2 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER SYSTEM OVERVIEW 1 COSPAS SARSAT System A Description Launched in the early eighties by the four founder countries Canada France Russia USA the COSPAS SARSAT system provides satellite aid to search and rescue SAR operations for maritime aeronautical and terrestrial vehicles anywhere in the world It uses distress beacons fitted on mobiles and a constellation of LEO and GEO satellites which relay and process the 406 MHz signal to ground stations LUT where the beacon positions are determined with a precision of less than 2 NM Several types of beacons are designe
32. te that no transmission must be interrupted unless every means are used to contact and inform the Air Traffic Controller of this action Important notice As 406 MHz transmission is effective 50 seconds after the ELT activation if it is switched off within this delay no further radio contact will be necessary 5 Self Test Refer to 1 Self test page 301 PAGE 107 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 6 Compatibility list A Mounting brackets Designation Part Number COMPACT MOUNTING BRACKET KIT 51840502 01 COMPACT UNIVERSAL MOUNTING BRACKET KIT 51840502 02 Remote control panels RCP Designation Part Number RC100 KIT 51820513 03 200 51820513 11 RC200 NVG 51820513 14 RC102 KIT 51820513 21 DIN 12 connector or programming dongles Designation Part Number DIN 12 connector 51820514 03 Programming dongle 51820514 01 Programming dongle Assy 51820514 06 D Outside antennas KANNAD Designation Manufacturer KANNAD Part Number ANT200 DAYTON GRANGER 0145621 ELT 10 773 x ANT300 CHELTON 1327 82 0124220 WHIP ANT AV200 RAMI AV 200 0146150 ROD ANT AV300 RAMI AV 300 0146151 ANT100 See note PROCOM 0124206 NOTE ANT100 is a non ETSO TSO antenna It may be used as auxiliary antenna if the ELT is used as portable equipment and if such a use is approved by local authorities PAGE 108 MAY 05 2010 INSTALLATION MANUAL OPERATION MANUAL INS
33. used for our beacon and battery pack any corrosions between two battery replacements is unlikely to happen However if this inspection is required by Civil Aviation Authority this check is detailed in CMM 25 63 03 page block CHECK page 5001 Note 1 As indicated in the Canadian operating rule Standard 625 the ELT shall be checked at intervals not exceeding 12 months in accordance with Appendix of Chapter 571 of the Airworthiness Manual 1 Proper installation Remove ELT from its mounting bracket Refer to 6 Removal page 207 Inspect the mounting bracket and the ELT Ensure the mounting bracket and the ELT are free of cracks or other obvious damage Inspect the connection Visually inspect all connector pins 2 Operation of the control crash sensor Refer to CMM 25 63 03 page block TESTING AND FAULT ISOLATION TASK 25 63 03 700 801 01 Beacon operating tests PAGE 601 SEP 16 2009 INSTALLATION MANUAL OPERATION MANUAL KANNAD ELT KANNAD 406 AF COMPACT 406 AF COMPACT ER 3 Transmitted signals Refer to CMM 25 63 03 page block TESTING AND FAULT ISOLATION TASK 25 63 03 700 801 01 Beacon operating tests or Refer to B 406 and 121 5 MHz transmission test page 302 4 Batteries corrosion Refer to CMM 25 63 03 page block CHECK TASK 25 63 03 700 801 01 Beacon operating tests 5 Check of 121 5 MHz frequency Re install the ELT Refer to 3 ELT transmitter installation procedure page 204
34. y available from any KANNAD distributor or dealer List of distributor available on our Web site http www kannad com KANNAD 2 1 des Cinq Chemins BP23 56520 GUIDEL FRANCE Telephone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 Web http www kannad com E mail contact aviation kannad com Support support sar kannad com Tel 33 0 2 97 02 49 00 PAGE 604 SEP 16 2009 Distributed by Manufactured by KANNA KANNAD 2 1 des Cinq Chemins BP23 56520 GUIDEL FRANCE T l Phone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 DOC08038D Ref 0145599D
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