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INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG

KANNAD 406 AP-H

PAGE INTRO 1

JUL 24/2013

INTRODUCTION

The instructions in this manual provide the information necessary for the
installation and the operation of KANNAD 406 AP-H ELT.

Servicing instructions (

Refer to SERVICING page 601

) are normally performed

by shop personnel.

For servicing and maintenance instructions, refer to relevant CMM.

For regulatory requirements, please consult your national aviation authority.

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Summary of Contents for 406 AP-H

Page 1: ...02 04 KANNAD 406 AP H transmitter P N S1820511 01 Mounting bracket 1 strap P N 0124206 ANT100 auxiliary antenna Orolia S A S This document is the property of Orolia S A S and contains proprietary and confidential information The document is loaned on the express condition that neither the document itself nor the information contained therein shall be disclosed without the express consent of Orolia...

Page 2: ...Users are kindly requested to notify Orolia S A S of any discrepancy omission or error found in this manual Please report to our customer support E mail support sar orolia com Tel 33 0 2 97 02 49 00 ...

Page 3: ...406 AP H RECORD OF REVISIONS ROR PAGE 1 JUL 24 2013 REV Nb REVISION DATE INSERTION DATE BY 00 OCT 18 2006 OCT 18 2006 J S 01 FEB 13 2008 FEB 13 2008 J S 02 SEP 12 2008 SEP 12 2008 J S 03 APR 30 2010 APR 30 2010 J S 04 JUL 24 2013 JUL 24 2013 J S ...

Page 4: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H RECORD OF REVISIONS ROR PAGE 2 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 5: ... 2 JUL 24 2013 List of Effective Pages LEP 1 JUL 24 2013 LEP 2 JUL 24 2013 Table of Contents TOC 1 JUL 24 2013 TOC 2 JUL 24 2013 TOC 3 JUL 24 2013 TOC 4 JUL 24 2013 Introduction INTRO 1 JUL 24 2013 INTRO 2 JUL 24 2013 System Overview 1 JUL 24 2013 2 JUL 24 2013 3 JUL 24 2013 4 JUL 24 2013 5 JUL 24 2013 6 JUL 24 2013 7 JUL 24 2013 8 JUL 24 2013 System Functional Description and Operation ...

Page 6: ... 105 JUL 24 2013 106 JUL 24 2013 107 JUL 24 2013 108 JUL 24 2013 109 JUL 24 2013 110 JUL 24 2013 Installation Removal 201 JUL 24 2013 202 JUL 24 2013 203 JUL 24 2013 204 JUL 24 2013 205 JUL 24 2013 206 JUL 24 2013 207 JUL 24 2013 208 JUL 24 2013 209 JUL 24 2013 210 JUL 24 2013 Check 301 JUL 24 2013 302 JUL 24 2013 303 JUL 24 2013 304 JUL 24 2013 SUBJECT PAGE DATE ...

Page 7: ...P PAGE 3 JUL 24 2013 Troubleshooting 401 JUL 24 2013 402 JUL 24 2013 Schematics and Diagrams 501 JUL 24 2013 502 JUL 24 2013 503 JUL 24 2013 504 JUL 24 2013 505 JUL 24 2013 506 JUL 24 2013 507 JUL 24 2013 508 JUL 24 2013 Servicing 601 JUL 24 2013 602 JUL 24 2013 SUBJECT PAGE DATE ...

Page 8: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H LIST OF EFFECTIVE PAGES LEP PAGE 4 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 9: ...control panels RCP 6 DIN 12 connector or programming dongles 6 ELT NAV System Interface 6 External antennas 7 SYSTEM FUNCTIONAL DESCRIPTION AND OPERATION 101 Transmitter 101 Controls 102 Working mode information 103 Off 103 Self Test 103 Armed 104 On 104 Autonomy 105 Electrical characteristics 106 Electrical interface 106 Technical Specifications 107 Activation 108 Standby mode for automatic activ...

Page 10: ...location 208 Antenna installation procedure 208 First power up 210 Removal 210 CHECK 301 Self test 301 Periodicity 301 Self test procedure 301 ELT operational tests 302 Installation without programming dongle 302 Installation with Programming Dongle 302 RCP operational tests 303 406 and 121 5 MHz transmission test 304 ELT Antenna link 304 406 MHz 304 121 5 MHz 304 TROUBLESHOOTING 401 General 401 F...

Page 11: ...3 ANT AV200 outline dimensions and drilling mask 504 ANT AV300 outline dimensions and drilling mask 505 ANT300 outline dimensions and drilling mask 506 ANT 410 outline dimensions and drilling mask 507 SERVICING 601 Maintenance Schedule 601 Periodic inspection 601 Every 6 years 601 Battery replacement 602 ...

Page 12: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H TABLE OF CONTENTS TOC PAGE 4 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 13: ...anual provide the information necessary for the installation and the operation of KANNAD 406 AP H ELT Servicing instructions Refer to SERVICING page 601 are normally performed by shop personnel For servicing and maintenance instructions refer to relevant CMM For regulatory requirements please consult your national aviation authority ...

Page 14: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AP H PAGE INTRO 2 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 15: ...ted on mobiles and a constellation of LEO and GEO satellites which relay the 121 5 243 MHz signals and process the 406 MHz signal to ground stations LUT where the beacon positions are determined with a precision of 10 NM with 121 5 243 signals and less than 2 NM with 406 signals Several types of beacons are designed to match the various applications of the COSPAS SARSAT system EPIRB Emergency Posi...

Page 16: ...nd 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 C 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 antideflagration extreme temperatures 20 C to 55 C fo...

Page 17: ...efer to RTCA DO 183 RTCA DO 204 EUROCAE ED 62 4 an outside antenna 5 a Programming Dongle for pin programming function option 6 CS144 Interface Module option 7 an auxiliary antenna for use as a survival beacon The transmitter bracket Programming Dongle and CS144 Interface Module are installed in the aircraft near the tail The outside antenna is mounted on the fuselage near the tail The remote cont...

Page 18: ... of the ELT for maintenance or exchange C Remote Control Panel A remote control panel can be supplied for installation in the cockpit in order to enable the pilot to monitor and control the ELT status The following controls are to be found on the panel 3 position switch ON ARMED RESET TEST red or amber visual indicator beeper on certain versions The remote control panel is connected to the ELT via...

Page 19: ...AGE 5 JUL 24 2013 4 Design features The KANNAD 406 AP H is made of moulded plastic with excellent mechanical resistance ASA PC light yellow colour The housing is designed with no sharp edges Figure 3 KANNAD 406 AP H with mounting bracket ANT ARM OFF ON RC ...

Page 20: ...VG S1820513 14 RC300 S1820513 09 RC400 S1820513 05 RC500 320 S1820513 02 RC600 NVG Y S1820513 12 RC600 NVG W S1820513 13 RC800 S1820513 15 RC810 S1820513 23 Orolia Designation Orolia Part Number DIN 12 connector S1820514 03 Programming dongle S1820514 01 Programming dongle A320 S1820514 04 Programming dongle A330 340 S1820514 05 Programming dongle Assy S1820514 06 Orolia Designation Orolia Part Nu...

Page 21: ...olia Designation Manufacturer Orolia Part Number ANT560 DAYTON GRANGER ELT 10 696 1 0145787 ANT410 DAYTON GRANGER ELT 720063 0145488 ANT300 CHELTON 1327 82 0124220 ANT AV200 RAMI AV 200 0146150 ANT AV300 RAMI AV 300 0146151 N A ARTEX 110 340 N A N A HR SMITH 10 118 32 N A N A COBHAM 2632 82 N A ...

Page 22: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 8 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 23: ...recise pinpointing and identification of the aircraft in distress Once activated the transmitter operates continuously on 121 5 and 243 0 MHz with an output power of 100 mW on each frequency The modulation is an audio frequency sweeping downwards from 1420 Hz to 490 Hz with a repetition rate of 3 Hz During the first 24 hours of operation a digital message is transmitted on 406 025 MHz every 50 sec...

Page 24: ...pment 4 BNC connector for the antenna Figure 101 Front Panel The red visual indicator gives an indication on the working mode of the beacon after the self test a series of short flashes indicate the self test failed one long flash indicates a correct self test in operating mode periodic flashes during 121 5 243 transmission long flash during 406 transmission A buzzer gives audio information on the...

Page 25: ...ics of the transmitter Battery voltage Programming and enables digital communication with a programming and test equipment This mode is selected when switching from OFF to ARM when switching to RESET TEST on the Remote Control Panel provided that the switch of the ELT is in the ARM position when switching to ON prior to transmission The buzzer operates during the self test procedure After about 3 ...

Page 26: ...g the Remote Control Panel switch to position ON provided that the ELT switch is in the ARM position when a crash occurs provided that the ELT switch is in the ARM position When this mode is selected the ELT starts transmission on 121 5 MHz 243 MHz immediately continuous transmission on 406 MHz after 50 seconds 406 burst every 50 sec during 24 hours The red visual indicator on the ELT and on the r...

Page 27: ... 5 243 MHz homing frequency transmission for the rescue operations the 406 MHz transmission is deliberately stopped after 24 hours to extend the 121 5 243 transmission for as long as possible 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 every 6 years see note below NOTE The useful lif...

Page 28: ...d or to the programming equipment PR600 IMPORTANT Shielded cables are recommended The required wires are AWG24 Table 1 J1 connector pin out This wire is not used with some versions of Remote Control Panels For precise information refer to Remote Control Panel technical description J2 Connector J2 is used to connect the external antenna through a 50 Ω coaxial cable for use as fixed ELT or the auxil...

Page 29: ...0 Hz to 490 Hz with decreasing sweep Autonomy Over 48 hours at 20 C CONTROLS ARM OFF ON switch Bright red visual indicator BNC antenna connector DIN12 connector for remote control panel RCP and pin programming option Buzzer G SWITCH SENSOR Mechanical G switch sensor at 45 compliant with EUROCAE ED62 specifications BATTERY KIT BAT300 P N S1820516 99 3 x LiMnO2 D type cells for transmitter power sup...

Page 30: ...e ELT switch is in the ARM position B Manual activation as fixed ELT Check that the external antenna is correctly connected Switch to ON either on the ELT or on the Remote Control Panel The ELT starts with the self test sequence 121 5 243 MHz transmission starts immediately after the self test 406 MHz starts after 50 seconds 406 burst every 50 sec during 24 hours During transmission buzzer operate...

Page 31: ...econds During transmission buzzer operates and visual indicator flashes periodically 8 Reset It is possible to stop the ELT in case of unintentional activation Important notice As 406 MHz transmission is effective 50 seconds after the ELT activation if it is reset within this delay no further radio contact will be necessary A Manual reset Switch to OFF B Reset with Remote Control Panel The switch ...

Page 32: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 110 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 33: ...ation The identification is simply downloaded in the ELT when connected to the programming equipment via the DIN 12 connector A Pin programming option The KANNAD 406 AP H offers pin programming capabilities to facilitate maintenance operations especially in case of removals and or replacement A special DIN 12 connector with a Serial Memory Module called Programming Dongle is connected to the ELT w...

Page 34: ...e 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 on board 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 the 6 digits of the CSN number If the pin programming ...

Page 35: ... determine that the aircraft installation conditions are within the TSO standards TSO articles must have separate approval for installation in an aircaft The article may be installed only according to 14 CFR part 43 of the applicable airworthiness requirements 3 RTCA DO 182 Recommandations All ELT system components which must survive to a crash intact should be attached to the airframe in such a m...

Page 36: ...of 15 If the KANNAD 406 AP H is installed with the Direction of Flight arrow pointing towards the front of the helicopter the ELT shall be mounted with the upper side pointing towards the top of the helicopter If the KANNAD 406 AP H is installed with the Direction of Flight arrow pointing towards the bottom of the helicopter the ELT shall be installed with the lower side pointing towards the front...

Page 37: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 205 JUL 24 2013 Figure 203 Bracket installation ...

Page 38: ...et CAUTION AN INCORRECT TIGHTENING OF THE HOOK AND LOOP FASTENER COULD LEAD TO AN UNSAFE SITUATION BY THE ELT PREVENTING THE TRANSMISSION OF THE DISTRESS MESSAGE IMPORTANT Once installed in the mounting bracket the installer must be sure that the transmitter is firmly attached in its bracket by trying to extract it manually thereby verifying there is no play and that it remains attached when extra...

Page 39: ...ructions for an external antenna installation are detailed 3 Antenna Installation page 208 Connect the Remote Control Panel or CS144 to the DIN12 connector Refer to Figure 205 Installation controls and connectors as shown Figure 2 ELT system description page 3 Set the 3 position switch Refer to Figure 205 Installation controls and connectors to ARM Figure 205 Installation controls and connectors P...

Page 40: ...e vertically polarized when the aircraft is in the normal flight attitude ELT antenna mounting surface should be able to whistand a static load equal to 100 times the antenna weight applied at the antenna mounting base in all directions The antenna should be mounted as close to the respective ELT as applicable The proximity of the ELT antenna to any vertically polarized communications antenna shal...

Page 41: ...adial should be at least equal to the antenna length and width at least 1 inch due to the diameter of the antenna The ground plane must be connected to the shield of the antenna connector Figure 206 Antenna ground plane for non metallic aircraft According to the antenna to be installed use the appropriate outline drawings and drilling masks to determine the hole patern and drill size Refer to SCHE...

Page 42: ... 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 or manually by RCP if any Note switching to ON directly on the ELT front panel will also activate the ELT 5 Removal Switch the ELT to OFF Refer to Figure 205 Installation controls and connectors Disconnect the Remote Control Panel or CS144 from the DIN12 connector Refer to Fi...

Page 43: ...position OFF to position ARM or press RESET TEST on the Remote Control Panel ensure that the ELT switch is in the ARM position The buzzer operates during the whole Self test procedure After a few seconds the test result is displayed with the visual indicator as follows One long flash indicates that the system is operational and that no error conditions were found A series of short flashes see Rema...

Page 44: ...ing Dongle connect the outside antenna to J2 switch the ELT from OFF to ARM check that the Self Test fails 3 4 flashes if not connect a maintenance dongle to J1 Switch the ELT from OFF to ARM Check that the Self Test fails 3 4 flashes Remove the maintenance dongle from J1 connect the Programming Dongle to J1 switch the ELT from OFF to ARM the buzzer operates during the whole self test procedure af...

Page 45: ...l tests Check correct operation of RCP LED and external buzzer by switching ELT and RCP as described in the sequential procedure hereunder with ELT switch in the ARM position Figure 301 RCP LED and buzzer operation IMPORTANT 2 before switching the RCP to ON wait for the end of the self test ...

Page 46: ... to the programmed message NOTE The message transmitted during self test sequence always begins with FF FE D0 whereas a programmed message begins with FF FE 2F Example of message programmed in ELT FF FE 2F 53 C3 24 97 38 0B A6 0F D0 F5 20 Example of same message decoded by SARTECH ARG5410 FF FE D0 53 C3 24 97 38 0B A6 0F D0 F5 20 C 121 5 MHz IMPORTANT this test must only be carried out between H a...

Page 47: ...r refer to relevant CMM for tests and repair 3 3 3 flashes Faulty VCO locking faulty frequency Check 406 MHz frequency refer to relevant CMM for tests and repair 4 3 4 flashes No identification programmed refer to relevant CMM for tests and repair Note for CMM download and other servicing instructions refer to Service Support section of Kannad Aviation Web site http www kannadaviation com 3 Other ...

Page 48: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 402 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 49: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 501 JUL 24 2013 SCHEMATICS DIAGRAMS 1 Outline Dimensions Note all dimensions are in millimeters inches in bracket ...

Page 50: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 502 JUL 24 2013 2 Drilling Mask ...

Page 51: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 503 JUL 24 2013 3 Wiring ...

Page 52: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 504 JUL 24 2013 4 ANT AV200 outline dimensions and drilling mask ...

Page 53: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 505 JUL 24 2013 5 ANT AV300 outline dimensions and drilling mask ...

Page 54: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 506 JUL 24 2013 6 ANT300 outline dimensions and drilling mask ...

Page 55: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 507 JUL 24 2013 7 ANT 410 outline dimensions and drilling mask ...

Page 56: ...INSTALLATION MANUAL OPERATION MANUAL KANNAD 406 AP H PAGE 508 JUL 24 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 57: ...ming kit required NOTE This functioning check can be carried out without opening the ELT These tests are described in Service Letter SL S18XX502 25 12 B Every 6 years Testing of the various elements of the ELT is mandatory every 6 years together with the battery replacement Visual control of the housing and accessories Refer to CMM 25 63 01or CMM 25 63 05 O ring battery and desiccant capsule repla...

Page 58: ...on distributor or dealer List of distributor available on our Web site http www kannadaviation com Orolia S A S Z I des Cinq Chemins CS10028 56520 GUIDEL FRANCE Telephone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 Web http www kannadaviation com E mail contact kannadaviation com Support support sar orolia com Tel 33 0 2 97 02 49 00 Only original battery pack included in battery kit KIT BAT 300 P N ...

Page 59: ......

Page 60: ...0143020E Distributed by Manufactured by Orolia S A S Z I des Cinq Chemins CS10028 56520 GUIDEL FRANCE Tél Phone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 Web http www kannadaviation com A Company of the Orolia Group ...

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