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INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG

KANNAD 406 AF / AF-H / AF (6D)

PAGE: 208

JUN 23/2008

C. KANNAD 406 AF (6D) installation

Figure 207: KANNAD 406 AF (6D) installation

For fixed wings aircraft and helicopters, the KANNAD 406 AF (6D) shall be
mounted in roll or pitch plane, either parallel or perpendicular to the aircraft
flight direction.

4. First power up

Perform the following tests:

1.

ELT operational tests:

Refer to 2. ELT operational tests, page 302

2.

RCP operational tests:

Refer to 3. RCP operational tests, page 303

3.

406 & 121.5 MHz transmission tests (optional):

Refer to 4. 406 and 121.5 MHz transmission test, page 304

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Summary of Contents for 406 AF

Page 1: ...F 6D transmitter P N S1820511 01 Mounting bracket 1 strap KANNAD This document is the property of KANNAD 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 KANNAD and that the information shall not be used by the recipient witho...

Page 2: ...Users are kindly requested to notify KANNAD for any discrepancy omission or error found in this manual Please report to our customer support E mail support sar kannad Tel 33 0 2 97 02 49 00 ...

Page 3: ...NS ROR PAGE 1 JUN 23 2008 REV Nb REVISION DATE INSERTION DATE BY 01 02 03 04 05 06 OCT 14 2003 OCT 14 2003 J S 07 NOV 19 2003 NOV 19 2003 J S 08 APR 23 2004 APR 23 2004 J S 09 JAN 24 2005 JAN 24 2005 J S 10 JUN 27 2005 JUN 27 2005 J S 11 FEB 01 2008 FEB 01 2008 J S 12 JUN 23 2008 JUN 23 2008 J S ...

Page 4: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D RECORD OF REVISIONS ROR PAGE 2 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 5: ...3 2008 ROR 2 JUN 23 2008 List of Effective Pages LEP 1 JUN 23 2008 LEP 2 JUN 23 2008 Table of Contents TOC 1 JUN 23 2008 TOC 2 JUN 23 2008 TOC 3 JUN 23 2008 TOC 4 JUN 23 2008 Introduction INTRO 1 JUN 23 2008 INTRO 2 JUN 23 2008 System Overview 1 JUN 23 2008 2 JUN 23 2008 3 JUN 23 2008 4 JUN 23 2008 5 JUN 23 2008 6 JUN 23 2008 System Functional Description and Operation 101 JUN 23 2008 102 JUN 23 2...

Page 6: ... JUN 23 2008 106 JUN 23 2008 107 JUN 23 2008 108 JUN 23 2008 Installation Removal 201 JUN 23 2008 202 JUN 23 2008 203 JUN 23 2008 204 JUN 23 2008 205 JUN 23 2008 206 JUN 23 2008 207 JUN 23 2008 208 JUN 23 2008 209 JUN 23 2008 210 JUN 23 2008 Check 301 JUN 23 2008 302 JUN 23 2008 303 JUN 23 2008 304 JUN 23 2008 Troubleshooting 401 JUN 23 2008 SUBJECT PAGE DATE ...

Page 7: ...TION LOG KANNAD 406 AF AF H AF 6D LIST OF EFFECTIVE PAGES LEP PAGE 3 JUN 23 2008 402 JUN 23 2008 Schematics and Diagrams 501 JUN 23 2008 502 JUN 23 2008 503 JUN 23 2008 504 JUN 23 2008 Servicing 601 JUN 23 2008 602 JUN 23 2008 SUBJECT PAGE DATE ...

Page 8: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D LIST OF EFFECTIVE PAGES LEP PAGE 4 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 9: ... 4 Remote Control Panel 4 Outside antenna 4 Design features 5 General 5 Mechanical design 5 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 activation 108 Manual a...

Page 10: ...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 Faults on Self test 401 Visual indicator 401 3 1 flashes 401 3 2 flashes 401 3 3 flashes 401 3 4 flashes 401 Other faults detected 401 Buzzer 401 Bu...

Page 11: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D TABLE OF CONTENTS TOC PAGE 3 JUN 23 2008 Periodic inspection 601 Every 6 years 601 Battery replacement 602 ...

Page 12: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D TABLE OF CONTENTS TOC PAGE 4 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 13: ...s in this manual provide the information necessary for the installation and the operation of KANNAD 406 AF AF H and AF 6D ELTs Servicing instructions are normally performed by shop personnel For servicing and maintenance instructions refer to CMM 25 63 01 For regulatory requirements please consult your national aviation authority ...

Page 14: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE INTRO 2 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 15: ... beacons fitted 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 Em...

Page 16: ...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 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 t...

Page 17: ... antenna 5 a Programming Dongle for pin programming function option 6 CS144 Interface Module option 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 control panel is installed in the cockpit and connected to the ELT with a 4 or 5 wire bundle Figure 2 ELT system d...

Page 18: ...nance or exchange C Remote Control Panel A remote control panel is available 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 a 4 or 5 wire cable equi...

Page 19: ... 406 AF AF H AF 6D belong to the AF type of ELTs which are permanently attached to an aircraft B Mechanical design The KANNAD 406 AF AF H AF 6D are 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 AF AF H AF 6D with mounting bracket ...

Page 20: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 6 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 21: ...ellites for precise 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...

Page 22: ...ogramming equipment 4 BNC connector for the antenna Figure 101 Front Panel The 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 informat...

Page 23: ...he ELT checks the main characteristics 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...

Page 24: ... selected manually by switching to position ON by switching the Remote Control Panel switch to ON provided that the ELT switch is in the ARM position when a crash occurs provided that the ELT switch is in position ARM 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...

Page 25: ...er for 121 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 ...

Page 26: ...or Maintenance Dongles to the CS144 interface and 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 outside antenna through a 50 Ω ...

Page 27: ...ency Modulation type 3K20A3X Modulation rate between 85 and 100 Frequency of modulation signal 1420 Hz to 490 Hz with decreasing sweep Autonomy Over 48 hours at 20 C CONTROLS ARM OFF ON switch Red visual indicator BNC antenna connector DIN12 connector for remote control panel and pin programming option Buzzer G SWITCH SENSOR Mechanical G switch sensor compliant with EUROCAE ED62 specifications 6 G...

Page 28: ...ote 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 MHz burst every 50 sec during 24 hours During transmission buzzer operates and visual indicator flashes 8 Reset It is possible to stop the ELT in case of unintentional activation Important notice As 406 MHz transmission is effective 50 s...

Page 29: ...eads longerons spars or floor beams not aircraft skin The mounts shall have a maximum static local deflection no greater than 2 5 mm 0 1 inch when a force of 450 Newton 100 lbf is applied to the mount in the most flexible direction Deflection measurements shall be made with reference to another part of the airframe not less than 0 3 meters 1 foot nor more than 1 0 meter 3 feet from the mounting lo...

Page 30: ... downloaded in the ELT when connected to the KANNAD programming equipment via the DIN 12 connector A Pin programming option The KANNAD 406 AF AF H AF 6D offer 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 when installed on bo...

Page 31: ...ansmission 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 option is selected by t...

Page 32: ...tion page 208 Drill 4 holes Ø 6 mm in the aircraft structure according to Drilling mask Holes 4 5 6 7 shall be preferred If the aircraft structure is not solid enough to withstand a 500 kg traction on the bracket a reinforcement plate not supplied should be installed as shown Figure 202 Bracket installation Fix the bracket with the 4 screws 8 washers and 4 nylstop nuts supplied IMPORTANT tighten t...

Page 33: ...ure 2 ELT system description page 3 Note regarding the outside antenna The installation of the outside antenna is not covered by this manual Refer to antenna manufacturer s instructions If the aircraft is not metallic the antenna should be mounted on a metallic counterpart Connect the Remote Control Panel or CS144 to the DIN12 connector Refer to Figure 204 Installation controls and connectors as s...

Page 34: ...uently the KANNAD 406 AF shall be mounted with the arrow of the Direction of Flight label pointed towards the front of the aircraft 2 Helicopters The KANNAD 406 AF can be installed in its standard version on helicopter The ELT unit should be mounted with the front face connectors pointing downwards at a 45 angle to the yaw axis and with Direction of Flight arrow towards the front of the helicopter...

Page 35: ...t towards the front or the bottom of the helicopter and not pointing 45 downwards If the KANNAD 406 AF 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 AF H is installed with the Direction of Flight arrow pointing towards the bottom of the helicopt...

Page 36: ...ters the KANNAD 406 AF 6D shall be mounted in roll or pitch plane either parallel or perpendicular to the aircraft flight direction 4 First power up Perform the following tests 1 ELT operational tests Refer to 2 ELT operational tests page 302 2 RCP operational tests Refer to 3 RCP operational tests page 303 3 406 121 5 MHz transmission tests optional Refer to 4 406 and 121 5 MHz transmission test ...

Page 37: ...trols and connectors Disconnect the Remote Control Panel or CS144 from the DIN12 connector Refer to Figure 204 Installation controls and connectors Disconnect the outside antenna from the BNC connector Refer to Figure 204 Installation controls and connectors Unfasten the self stripping strap Remove the transmitter from the bracket Figure 208 Removing the transmitter ...

Page 38: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 210 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 39: ...Switch from 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 flas...

Page 40: ...ith programming 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 ...

Page 41: ...P operational 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 42: ...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 and H 5 m...

Page 43: ...efer to CMM 25 63 01 for repair see note 1 below 2 3 2 flashes Low RF power Check 406 MHz power refer to CMM 25 63 01 for repair see note 1 below 3 3 3 flashes Faulty VCO locking faulty frequency Check 406 MHz frequency refer to CMM 25 63 01 for repair see note 1 below 4 3 4 flashes No identification programmed Check programming see note 2 below NOTE 1 Only PART FAR 145 certified stations accredit...

Page 44: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 402 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 45: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 501 JUN 23 2008 SCHEMATICS DIAGRAMS 1 Outline Dimensions ...

Page 46: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 502 JUN 23 2008 2 Drilling Mask ...

Page 47: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 503 JUN 23 2008 3 Wiring ...

Page 48: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF AF H AF 6D PAGE 504 JUN 23 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 49: ...ions optional programming kit required Number of self tests carried out optional programming kit required Programmed data optional programming kit required NOTE This functioning check can be carried out without opening the ELT 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 Ref...

Page 50: ...r or dealer KANNAD Z I 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 List of distributor available on our Web site http www kannad com Only original battery pack included in battery kit KIT BAT 300 P N S1820516 99 supplied by KANNAD can be...

Page 51: ......

Page 52: ...DMA174N Ref 0139162N Distributed by Manufactured by KANNAD Z I des Cinq Chemins BP23 56520 GUIDEL FRANCE Tél Phone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 Web http www kannad com ...

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