Kannad AF INTEGRA Operation Manual Download | Manualshive

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OPERATION MANUAL

AF INTEGRA / AF-H INTEGRA ELT

PAGE: 501

JUN 20/2013

SCHEMATICS & DIAGRAMS

1. Outline dimensions and weight with mounting bracket AF-COMPACT

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Summary of Contents for AF INTEGRA

Page 1: ...ocument 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 S A S and that the information shall not be used by the recipient without prior written acceptance by Orolia S A S Furthermore the...

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: ...GRA AF H INTEGRA ELT RECORD OF REVISIONS ROR PAGE 1 JUN 20 2013 REV Nb REVISION DATE INSERTION DATE BY 00 OCT 20 2010 OCT 20 2010 J S 01 MAY 09 2011 MAY 09 2011 J S 02 JAN 31 2012 JAN 31 2012 J S 03 JUN 20 2013 JUN 20 2013 J S ...

Page 4: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT RECORD OF REVISIONS ROR PAGE 2 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 5: ... 20 2013 List of Effective Pages LEP 1 JUN 20 2013 LEP 2 JUN 20 2013 LEP 3 JUN 20 2013 LEP 4 JUN 20 2013 Table of Contents TOC 1 JUN 20 2013 TOC 2 JUN 20 2013 Introduction INTRO 1 JUN 20 2013 INTRO 2 JUN 20 2013 System Overview 1 JUN 20 2013 2 JUN 20 2013 3 JUN 20 2013 4 JUN 20 2013 5 JUN 20 2013 6 JUN 20 2013 System Functional Description and Operation 101 JUN 20 2013 102 JUN 20 2013 ...

Page 6: ... JUN 20 2013 108 JUN 20 2013 109 JUN 20 2013 110 JUN 20 2013 111 JUN 20 2013 112 JUN 20 2013 Installation Removal 201 JUN 20 2013 202 JUN 20 2013 203 JUN 20 2013 204 JUN 20 2013 205 JUN 20 2013 206 JUN 20 2013 207 JUN 20 2013 208 JUN 20 2013 Check 301 JUN 20 2013 302 JUN 20 2013 303 JUN 20 2013 304 JUN 20 2013 Troubleshooting 401 JUN 20 2013 SUBJECT PAGE DATE ...

Page 7: ... AF H INTEGRA ELT LIST OF EFFECTIVE PAGES LEP PAGE 3 JUN 20 2013 402 JUN 20 2013 Schematics and Diagrams 501 JUN 20 2013 502 JUN 20 2013 503 JUN 20 2013 504 JUN 20 2013 Servicing 601 JUN 20 2013 602 JUN 20 2013 SUBJECT PAGE DATE ...

Page 8: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT LIST OF EFFECTIVE PAGES LEP PAGE 4 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 9: ...n 101 Transmission 101 Controls Connectors 101 Working mode information 102 Off 102 Self Test 102 Armed 103 On 103 VSWR Switch function External Integral antenna 104 GPS Strategy 104 Basic Installation or portable use without NAV Interface equipment 104 Installation including a NAV Interface equipment Dongle IF GPS RS232 105 Autonomy 105 Electrical interfaces 106 Transmitter Technical Specificatio...

Page 10: ...perational tests 302 Test of transmitted signals 302 406 MHz Transmission tests 302 121 5 MHz Transmission tests 303 TROUBLESHOOTING 401 General 401 Faults on Self test 401 3 1 flashes 401 3 2 flashes 401 3 3 flashes 401 3 4 flashes 401 3 5 flashes 401 3 6 flashes 401 SCHEMATICS DIAGRAMS 501 Outline dimensions and weight with mounting bracket AF COMPACT 501 Outline dimensions and weight with unive...

Page 11: ...TEGRA is designed for flat installation on board helicopters only The AF INTEGRA ER and AF H INTEGRA ER ELTs are evolutions of AF INTEGRA and AF H INTEGRA ELTs The main evolution consists in the extension to 40 C of temperature range The instructions in this manual provide the information necessary for the installation and the operation of AF INTEGRA AF H INTEGRA AF INTEGRA ER and AF H INTEGRA ER ...

Page 12: ... identified as being defective by our services 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 cause...

Page 13: ...s 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 with the Doppler effect Several types of beacons are designed to match the various applications of the COSPAS SARSAT system EPIRB Emergency Position Indicating Radio Beacon f...

Page 14: ...ess 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 change of veloc...

Page 15: ...rol panel 1 5 a DIN 12 connector programming dongle or dongle IF GPS RS232 2 when the optional RCP is connected 6 an outside buzzer optional 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 readily accessible from the cockpit crew positio...

Page 16: ...GRA AF H INTEGRA ELT PAGE 4 JUN 20 2013 Figure 2 ELT system description Note Data position from an on board RS232 GPS only available if a dongle IF GPS RS232 5 is connected instead of programming dongle 5 or DIN 12 connector 5 ...

Page 17: ... 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 AF INTEGRA and AF H INTEGRA are certified as Automatic Fixed AF ELTs with the approved external antennas The housing of AF INTEGRA and AF H INTEGRA transmitters are made of molded plastic with excellent mechanical resistance The ELT housing is...

Page 18: ...acket P N S1840502 02 to re use existing drilling for retrofit Refer to DOC09081 Initial Installation Manual for drilling masks and outline dimensions of these brackets C External antenna Only approved antennas may be installed Refer to Section 6 Compatibility list page 110 Connection to the ELT will be carried out with a 50 Ohm coaxial cable RG58 for example ended with a male BNC connector IMPORT...

Page 19: ...ages 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 During operations a digital message is transmitted on 406 037 MHz every 50 seconds B Controls Connectors The following controls are to be found on the ELT front panel from...

Page 20: ...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 ...

Page 21: ...ed 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 ELT should remain in the ARM position except when the aircraft is parked for a ...

Page 22: ...programming and test equipment PR600 D VSWR Switch function External Integral antenna During the 406 MHz burst the Voltage Standing Wave Ratio VSWR is measured After 5 bursts with wrong VSWR measurements the ELT switches from the external to the internal antenna in order to optimize transmitted signal In ON mode after 36 bursts the ELT decides to re switch or not according to the result of 2 new V...

Page 23: ... 4 5 5 2 of Cospas Sarsat C S T001 if after providing valid data the navigation input fails or is not available the beacon message retains the last valid position for 4 hours 5 min after the last valid position data input After 4 hours the encoded position is set to the default values F Autonomy The energy is provided by a battery pack composed of a LiMnO2 two element battery See pages page 107 pa...

Page 24: ...1 J1 connector pin out J2 BNC female connector J2 is used to connect the external antenna through a 50 Ω coaxial cable IMPORTANT NOTICE The use of a low attenuation coaxial cable is recommended The maximum permitted attenuation in the coaxial is 1db 400 MHz J1 PIN Signal Name Destination Direction Viewed from Front Face J1 A RCP RESET RCP IN J1 B DONGLE RX SMM PGM IN J1 C DONGLE CS SMM OUT J1 D DO...

Page 25: ...R Mechanical G switch sensor compliant with EUROCAE ED62 specifications RF Fied strenght limits INTEGRA ER 0 471 V m INTEGRA 0 474 V m CONTROLS ARM OFF ON switch DIN12 socket for RCP and pin programming option Bright red visual indicator Buzzer BNC antenna connector BATTERY KIT BAT200 P N S1840510 01 LiMnO2 two element battery for transmitter power supply Battery expiry date 7 years from date of c...

Page 26: ... sf08792 html 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 Swit...

Page 27: ... 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 Section 1 Self test page 301 Regulations state that no transmission must be interrupted unless every means are used to contact and inform the Air Traffic Controller of this action ...

Page 28: ...NG BRACKET KIT S1840502 01 COMPACT UNIVERSAL MOUNTING BRACKET KIT S1840502 02 KANNAD Designation Part Number RC100 KIT S1820513 03 RC102 KIT S1820513 21 RC200 S1820513 11 RC300 S1820513 09 RC300 NVG S1820513 10 RC310 NVG S1820513 26 RC600 NVG Y S1820513 12 RC600 NVG W S1820513 13 RC800 S1820513 15 RC810 S1820513 23 Designation Part Number DIN 12 connector S1820514 03 Programming dongle S1820514 01...

Page 29: ... KANNAD Designation Manufacturer KANNAD Part Number ANT300 CHELTON 1327 82 0124220 WHIP ANT AV100 RAMI AV 100 0147444 WHIP ANT AV200 RAMI AV 200 0146150 ROD ANT AV300 RAMI AV 300 0146151 BLADE ANT500 SENSOR SYSTEMS S65 8282 406 0124222 BLADE ANT560 DAYTON GRANGER ELT10 696 1 0145787 BLADE ANT650 CHELTON 2624 82 0124251 N A CHELTON 2632 82 N A N A CHELTON 21 41 N A ...

Page 30: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 112 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 31: ...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 immedia...

Page 32: ...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 own...

Page 33: ...ates 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 ...

Page 34: ... of the ELT pointed towards the front or downwards the helicopter according to Section 4 AF H INTEGRA AF H INTEGRA ER axis of installation page 504 2 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 3 Fasten the self stripping strap tightly CAUTION AN ...

Page 35: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 205 JUN 20 2013 Figure 2 Installing the transmitter on the bracket ...

Page 36: ...ts 1 ELT operational tests connect the external antenna to J2 switch the ELT from OFF to ARM check that the Self Test result is OK one long flash 2 406 121 5 MHz transmission tests optional Refer to Section B Test of transmitted signals 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 Switc...

Page 37: ...o OFF 2 Disconnect the external antenna from the BNC connector of the ELT 3 If connected disconnect the DIN 12 Connector of Remote Control Panel bundle from the DIN12 socket of the ELT 4 Unfasten the self stripping strap 5 Remove the transmitter from the bracket Figure 4 Removing the transmitter ...

Page 38: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 208 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 39: ... 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 TEST on the Remote Contr...

Page 40: ...eck that the Self Test result is OK one long flash B Test of transmitted signals 1 406 MHz Transmission tests This test should be carried out with a COSPAS SARSAT decoder Note If a COSPAS SARSAT decoder is not available the coding sheet supplied by the programmer for the beacon or dongle with the corresponding CSN proves that the beacon or dongle is correctly programmed Skip to 2 121 5 MHz Perform...

Page 41: ...rsat decoder otherwise check 121 5 MHz using a VHF receiver not the on board VHF receiver several dozens meters away from the antenna This ensures to validate the antenna Tune VHF receiver to 121 5 MHz 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 ...

Page 42: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 304 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 43: ...ery voltage Replace battery refer to relevant CMM for tests and repair 2 3 2 flashes Low RF power Check 406 MHz power refer to relevant CMM for tests and repair 3 3 3 flashes Faulty VCO locking faulty frequency Check frequencies refer to relevant CMM for tests and repair 4 3 4 flashes No identification programmed Check programming refer to relevant CMM for tests and repair 5 3 5 flashes VSWR Fault...

Page 44: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 402 JUN 20 2013 PAGE INTENTIONALLY LEFT BLANK ...

Page 45: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 501 JUN 20 2013 SCHEMATICS DIAGRAMS 1 Outline dimensions and weight with mounting bracket AF COMPACT ...

Page 46: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 502 JUN 20 2013 2 Outline dimensions and weight with universal mounting bracket ...

Page 47: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 503 JUN 20 2013 3 AF INTEGRA AF INTEGRA ER axis of installation ...

Page 48: ...OPERATION MANUAL AF INTEGRA AF H INTEGRA ELT PAGE 504 JUN 20 2013 4 AF H INTEGRA AF H INTEGRA ER axis of installation ...

Page 49: ...ement Testing of various elements and parameters of the ELT is mandatory when the battery is replaced For battery replacement interval Refer to 2 Battery replacement requirements page 602 The testing procedure associated with the battery replacement is described in the relevant CMM For CMM download and other servicing instructions refer to Servcie Support section of Kannad Aviation Website Battery...

Page 50: ...lable 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 and approved battery pack included in battery KIT BAT200 P N S1840510 01 supplied by Orolia S A S can ...

Page 51: ......

Page 52: ...DOC09078D Ref 0146257D 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 A Company of the Orolia Group ...

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