Kannad 406 AF-COMPACT Installation Manual Download Page 32

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INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG

KANNAD 406 AF-COMPACT

PAGE: 112

FEB 01/2008

Table 3: D-SUB 9 Pts Male Characteristics

Table 4: D-SUB 9 Pts female, Mating Connector Characteristics

E. RC200 Technical Specifications

(1) Photovoltaic Relay

- Insulation: 1 KV

- Commutation 1A 60V

(2) Environmental specifications

- Operating temperature: - 20°C to + 55°C (DO160D section 4 category

A2).

- Storage temperature: - 55°C to + 85°C (DO160D section 4 category A2).

- Magnetic effect: According to DO-160D section 15 category Z.

Receptacle

Standard designation

D-SUB - Male - 9 Pts

Number of pins

Locking device

Inserts, Threaded UNC 4-40

KANNAD

0127012

Mating connector

Standard designation

D-SUB - Female - 9 Pts

Number of pins

KANNAD

S1840506-01

Summary of Contents for 406 AF-COMPACT

Page 1: ...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 without prior written acceptance by KANNAD Furthermore the document sh...

Page 2: ......

Page 3: ...SPECTION LOG KANNAD 406 AF COMPACT RECORD OF REVISIONS ROR PAGE 1 FEB 01 2008 REV Nb REVISION DATE INSERTION DATE BY 00 FEB 01 2007 FEB 01 2007 J S 01 SEP 04 2007 SEP 04 2007 J S 02 SEP 05 2007 SEP 05 2007 J S 03 FEB 01 2008 FEB 01 2008 J S ...

Page 4: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT RECORD OF REVISIONS ROR PAGE 2 FEB 01 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 5: ...2008 ROR 2 FEB 01 2008 List of Effective Pages LEP 1 FEB 01 2008 LEP 2 FEB 01 2008 Table of Contents TOC 1 FEB 01 2008 TOC 2 FEB 01 2008 TOC 3 FEB 01 2008 TOC 4 FEB 01 2008 Introduction INTRO 1 FEB 01 2008 INTRO 2 FEB 01 2008 System Overview 1 FEB 01 2008 2 FEB 01 2008 3 FEB 01 2008 4 FEB 01 2008 5 FEB 01 2008 6 FEB 01 2008 System Functional Description and Operation 101 FEB 01 2008 102 FEB 01 200...

Page 6: ... 2008 107 FEB 01 2008 108 FEB 01 2008 109 FEB 01 2008 110 FEB 01 2008 111 FEB 01 2008 112 FEB 01 2008 113 FEB 01 2008 114 FEB 01 2008 Installation Removal 201 FEB 01 2008 202 FEB 01 2008 203 FEB 01 2008 204 FEB 01 2008 205 FEB 01 2008 206 FEB 01 2008 207 FEB 01 2008 208 FEB 01 2008 209 FEB 01 2008 210 FEB 01 2008 211 FEB 01 2008 212 FEB 01 2008 213 FEB 01 2008 SUBJECT PAGE DATE ...

Page 7: ...08 303 FEB 01 2008 304 FEB 01 2008 Troubleshooting 401 FEB 01 2008 402 FEB 01 2008 Schematics and Diagrams 501 FEB 01 2008 502 FEB 01 2008 503 FEB 01 2008 504 FEB 01 2008 505 FEB 01 2008 506 FEB 01 2008 Servicing 601 FEB 01 2008 602 FEB 01 2008 603 FEB 01 2008 604 FEB 01 2008 605 FEB 01 2008 606 FEB 01 2008 607 FEB 01 2008 608 FEB 01 2008 609 FEB 01 2008 SUBJECT PAGE DATE ...

Page 8: ...PECTION LOG KANNAD 406 AF COMPACT LIST OF EFFECTIVE PAGES LEP PAGE 4 FEB 01 2008 610 FEB 01 2008 611 FEB 01 2008 612 FEB 01 2008 613 FEB 01 2008 614 FEB 01 2008 615 FEB 01 2008 616 FEB 01 2008 617 FEB 01 2008 618 FEB 01 2008 SUBJECT PAGE DATE ...

Page 9: ...CRIPTION AND OPERATION 101 Transmitter Functional Description 101 Transmission 101 Controls Connectors 102 Working mode information 103 Off 103 Self Test 103 Armed 104 On 104 Autonomy 105 Transmitter Technical characteristics 106 Mechanical characteristics 106 Material 106 Overall Dimensions 106 Weight 106 Electrical characteristics 106 Electrical interface 106 Transmitter Technical Specifications...

Page 10: ...ion in USA 201 Registration in Canada 202 Programming 203 Pin programming option 203 ELT Installation 204 ELT and bracket installation recommendations 204 FAA Recommendations 204 TSO C126 Paragraph D Requirements 204 RTCA DO 182 Recommandations 204 RTCA DO 204 Requirements 204 Bracket installation procedure 205 Fixed wing aircraft 205 Helicopters 205 ELT installation procedure 207 Antenna Installa...

Page 11: ...n Self test 401 Visual Indicator 401 3 1 flashes 401 3 2 flashes 401 3 3 flashes 401 3 4 flashes 401 SCHEMATICS DIAGRAMS 501 ELT Outline Dimensions 501 ELT Drilling Mask 502 RC200 Outline Dimensions 503 RC200 Drilling Mask 504 ANT200 Outline Dimensions 505 ANT300 Outline Dimensions 506 Wiring 507 SERVICING 601 Maintenance Schedule 601 Periodic inspection 601 Proper installation 601 Operation of th...

Page 12: ...OC PAGE 4 FEB 01 2008 Measurement of output powers frequencies and verification of digital message 603 Battery pack replacement 604 Check of 121 5 MHz frequency 609 Battery replacement requirements 610 Periodic Inspection Log 611to 619 Programming Log 620 to 623 Pre delivery Inspection Log 624 ...

Page 13: ...y for the installation and the operation of KANNAD 406 AF COMPACT ELT Servicing instructions of ELT are normally performed by shop personnel and detailed Section SERVICING page 601 For more detailed instructions and identification parts list refer to CMM 25 63 03 Servicing and maintenance instructions of RC200 RCP are detailed in ACMM 25 63 21 For a quick view of installation please refer to Quick...

Page 14: ...ir of the equipment or the element 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 Exclusi...

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 Eme...

Page 16: ...Ts 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 anti deflagration extreme temperatures 20 C to 55...

Page 17: ...a transmitter P N S1840501 01 2 a mounting bracket P N S1840502 01 3 an RC200 remote control panel P N S1820513 11 4 a DIN 12 connector P N S1820514 03 5 a SUB D 9 Pts Female connector P N S1840506 01 The approved outside whip P N 0141013 or rod P N 0124220 antennas are purchased separately The transmitter and bracket are installed in the aircraft near the tail The outside antenna is mounted on th...

Page 18: ...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 is certified as Automatic Fixed AF ELT and only works with the outside antennas described in this manual The housing of KANNAD 406 AF COMPACT transmitter is made of moulded plastic with excellent mechanical resistance Polycarbonate light yellow colour The ELT ...

Page 19: ...C Remote Control Panel An RC200 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 light The remote control panel is connected to the ELT via a 3 wire cable equipped with a DIN 12 connector on the ELT side and a D SUB Female...

Page 20: ...ype according to aircraft speed 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 electric properties similar to those of a RG58 cable Note the 50 Ohm coaxial cable and the male BNC connector are not supplied Figure 6 Whip and rod antennas ANT300 Rod Antenna ANT200 Whip Antenn...

Page 21: ...s 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 rat...

Page 22: ...r programming equipment 4 BNC connector for the antenna Figure 101 Front Panel The red light 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 transmission long flash during 406 transmission A buzzer gives audio information on ...

Page 23: ...aircraft 2 Self Test The self test mode is a temporary mode max duration 5 sec in which the ELT 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 the Remote Control Panel provided that the switch of the ELT is in pos...

Page 24: ...switch is on ARM position 4 On This mode is selected manually by switching the ELT to ON by switching the 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 1...

Page 25: ...e 406 MHz transmission of KANNAD 406 AF COMPACT is not stopped after 24 hours and 406 MHz transmission is continuing beyond 48 hours 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 life time of batteries is twelve 12 years To be in compliance ...

Page 26: ...ns page 501 Transmitter outline dimensions 131 x 86 x 75 4 mm 5 157 x 3 385 x 2 968 inches Outline dimensions with mounting bracket 140 x 98 x 86 4 mm 5 512 x 3 858 X 3 40 inches 4 Weight Typical 850 gr 1 874 lb Max 875 g r 1 929 lb 5 Electrical characteristics Transmitter power supply LiMnO2 two element battery 6 Electrical interface When installed onboard the ELT has to be connected to RC200 Rem...

Page 27: ...gh a 50 Ω coaxial cable IMPORTANT The length of the coaxial cable should not exceed 2 meters 6 ft for a standard RG58 or equivalent coaxial cable If the cable length exceeds 2 meters a low loss cable of attenuation less than 1 dB must be used See Important notice Section D Outside antenna page 6 J1 PIN Signal Name Destination Direction Viewed from Front Face J1 A RCP TEST RESET RCP IN J1 B DONGLE ...

Page 28: ... Bright red visual indicator BNC antenna connector DIN12 socket for remote control panel RCP and pin programming option Buzzer G SWITCH SENSOR Mechanical G switch sensor compliant with EUROCAE ED62 specifications BATTERY KIT BAT200 P N S1840510 01 LiMnO2 two element battery for transmitter power supply Replacement every 6 years HOUSING Material Polycarbonate Color Yellow color compounded Transmitt...

Page 29: ...0 enables the remote control of the primary functions of the KANNAD Emergency Locator Transmitters Manual activation Reset Test as well as visual monitoring B RC200 Controls and Connector The following elements are to be found on the RC200 Remote Control Panel 1 On Armed Reset Test a 3 position switch 2 Red led annunciator 3 J1 single male 9 pin D SUB connector 4 Warning stating FOR AVIATION EMERG...

Page 30: ... it in OFF position 2 Monitoring Monitoring is accomplished through a led operating in the same way as the ELT visual indicator Transmission 2 Hz pulsed signal during ELT transmission on 121 5 MHz 1 long flash during ELT transmission on 406 MHz every 50 seconds Self test 1 short flash at the beginning of the self test sequence 3 N flashes at the end of the self test sequence if the ELT is faulty N...

Page 31: ...lectrical Interfaces A single male 9 pin D SUB connector J1 enables to connect the RC200 remote control panel to the KANNAD 406 AF COMPACT with a 3 wire cable AWG 24 shielded recommended On the ELT side the wires are soldered to a male DIN 12 connector On the RCP side the wires are connected to a female 9 pin D SUB connector Note 1 RCP buzzer functionnality not featured by this model Table 2 J1 D ...

Page 32: ...ion 1 KV Commutation 1A 60V 2 Environmental specifications Operating temperature 20 C to 55 C DO160D section 4 category A2 Storage temperature 55 C to 85 C DO160D section 4 category A2 Magnetic effect According to DO 160D section 15 category Z Receptacle Standard designation D SUB Male 9 Pts Number of pins 9 Locking device Inserts Threaded UNC 4 40 KANNAD 0127012 Mating connector Standard designat...

Page 33: ...re 65 C to 71 C Connector BNC female Mount Ø 13 mm hole required 0 515 in Overall dimensions 634 5 x 25 mm max 24 98 x 1 in Antenna height 609 6 mm 24 in Speed rating 250 Knots Refer to 5 ANT200 Outline Dimensions page 505 2 ANT 300 Frequencies 121 5 243 406 MHz Impedance 50 ohms VSWR relative to 50 ohms 1 7 1 Weight 150 gr 0 33 lb Connector BNC female Overall dimensions 342 x 122 x 62 mm 13 47 x ...

Page 34: ...ote Control Panel 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 5 Reset It is possible to stop the ELT in case of unintentional activation Important notice As 406 MHz transmission is effective...

Page 35: ... 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 registratio...

Page 36: ... 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 ...

Page 37: ...utomatically 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 o...

Page 38: ... desiring to install this ELT on a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards The article may be installed only if further evaluation by the applicant documents an acceptable installation and it is approved by the Administrator 3 RTCA DO 182 Recommandations All ELT system components which must survive to a crash intact sho...

Page 39: ... Fixed wing aircraft The G Switch sensor axis shall be pointed to sense the primary crash pulse along the longitudinal axis of the aircraft with maximum tolerance of 15 Consequently the KANNAD 406 AF COMPACT shall be mounted with the arrow of the Flight direction label pointed towards the front of the aircraft 2 Helicopters The standard version of the KANNAD 406 AF COMPACT may be installed on heli...

Page 40: ... 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 203 Bracket installation Fix the bracket with the 4 screws 8 washers and 4 nylstop nuts supplied IMPORTANT tighten to a torque between 4 and 5 Newton x meter Verify that the ELT identification label matches the aircraft tail n...

Page 41: ...ointed towards the front of the aircraft Figure 202 KANNAD 406 AF COMPACT axis of installation 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 Figure 204 Installing the transmitter on the bracket ...

Page 42: ...l to 100 times the antenna s weight applied at the antenna mounting base along the longitudinal axis of the aircraft B Antenna mounting location The antenna must be mounted on the top of the aircraft to assure maximum visibility of satellites The upper aft portion of the fuselage should be preferred It should be mounted away from projections such as a propeller tail surfaces or the shadow of large...

Page 43: ...fabric or wood skin of the aircraft The length of each foil radial should be at least equal to the antenna length 0 61 meter 24 inches for ANT200 0 39 meter 15 47 inches for ANT300 Figure 205 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 5 ANT200 Ou...

Page 44: ...strument panel with 4 screws rivets bush recommended not supplied or below the instrument panel with a special mounting tray supplied 1 Installation on the instrument panel Determine RC200 location on the instrument panel Mark a cutout on the instrument panel according to the Drilling mask Refer to 4 RC200 Drilling Mask page 504 Make the cutout Mark the 4 holes needed for the RC200 using the drill...

Page 45: ...blished in RTCA DO 204 According to the area to be drilled 1 of the mounting tray 3 determine the location of the screws or rivets 2 used to secure the mounting tray 3 to the instrument panel 4 Drill 2 holes on the mounting tray and on the instrument panel diameter depending on screws or rivets used Secure the mounting tray 3 to the instrument panel 4 Secure the RC200 5 to the mounting tray 3 with...

Page 46: ... pack solder the wires to pins G RCP COMMON A RCP RESET and J RCP LED of the connector Put heat shrinkable sleeves to protect the pins On the RCP side Strap pins 4 and 5 of the female 9 pin D SUB connector supplied with the pack Solder the wires to the female 9 pin D SUB connector as follows Pin 8 RCP COMMON has to be connected to Pin G RCP COMMON of the ELT Pin 4 RCP RESET has to be connected to ...

Page 47: ...M 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 RCP to J1 and outside antenna to J2 switch the ELT from OFF to ARM check that the Self Test result is OK one long flash 2 RCP operational tests Refer to B RCP operational tests page 302 3 406 121 5 MHz transmission tests optional Re...

Page 48: ... Switch the ELT to OFF 2 Disconnect the outside antenna from the BNC connector of the ELT 3 Disconnect the DIN 12 Connector of Remote Control Panel 3 wire bundle from the DIN12 socket of the ELT 4 Unfasten the self stripping strap 5 Remove the transmitter from the bracket Figure 209 Removing the transmitter ...

Page 49: ...na is correctly connected Switch from position OFF to position ARM or press RESET TEST on the Remote Control Panel ensure that the ELT switch is in position ARM The buzzer operates during the whole Self test procedure After a few seconds the test result is displayed with the LED as follows One long flash indicates that the system is operational and that no error conditions were found A series of s...

Page 50: ...perational 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 RCP to J1 and outside antenna to J2 switch the ELT from OFF to ARM check that the Self Test result is OK one long flash B RCP operational tests Check correct operation of RCP LED annunc...

Page 51: ...s Sarsat Decoder FF FE D0 53 C3 24 97 38 0B A6 0F D0 F5 20 2 121 5 MHz This test must be carried out with a VHF receiver Aircraft VHF receiver may be used Tune VHF receiver to 121 5 MHz Start transmission either on ELT ON position or on the RCP ON position the ELT shall be in ARM position Listen to the two 121 5 MHz sweep tones during not more than the first five seconds then stop transmission see...

Page 52: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 304 FEB 01 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 53: ...y Refer to 4 Battery pack replacement page 604 2 3 2 flashes Low RF power Check 406 MHz power Refer to 3 Measurement of output powers frequencies and verification of digital message page 603 If power too low refer to CMM 25 63 03 for repair 3 3 3 flashes Faulty VCO locking faulty frequency Refer to 3 Measurement of output powers frequencies and verification of digital message page 603 If test fail...

Page 54: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 402 FEB 01 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 55: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 501 FEB 01 2008 SCHEMATICS DIAGRAMS 1 ELT Outline Dimensions ...

Page 56: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 502 FEB 01 2008 2 ELT Drilling Mask ...

Page 57: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 503 FEB 01 2008 3 RC200 Outline Dimensions ...

Page 58: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 504 FEB 01 2008 4 RC200 Drilling Mask ...

Page 59: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 505 FEB 01 2008 5 ANT200 Outline Dimensions ...

Page 60: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 506 FEB 01 2008 6 ANT300 Outline Dimensions ...

Page 61: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 507 FEB 01 2008 7 Wiring ...

Page 62: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 508 FEB 01 2008 PAGE INTENTIONALLY LEFT BLANK ...

Page 63: ...n be carried out without specific tools except a torque wrench with a 3 mm insert bit for hexalobular internal driving screws a 50 ohm load and the VHF tune receiver of the aircraft 1 Proper installation Remove ELT from its mounting bracket Refer to 8 Removal page 214 Inspect the mounting bracket and the ELT Ensure the mounting bracket and the ELT are free of cracks or other obvious damage Inspect...

Page 64: ...orrosion Refer to 4 Battery pack replacement page 604 to remove and re install the battery pack and check the watertightness of beacon Remove the battery pack from the ELT Inspect the battery pack The battery pack and connector should be free of corrosion Ensure the battery housing is free of cracks or other visible damage Verify the battery expiration date and ensure it matches with the expiratio...

Page 65: ...an be supplied by KANNAD under P N 0140956 or AEROFLEX IFR 4000 NAV COMM Ramp Test Set Other beacons testers can be used if they are capable to fill the functions required to measure power and frequencies of 121 5 and 406 MHz transmitters and to decode the digital message Refer to the applicable operation manual included with the test set 6 year inspection must be performed in the order listed bel...

Page 66: ...ital message coding Perform a self test B Self test procedure page 301 Check that except for the 5th and the 6th digits the decoder message is identical to the programmed message Note the message transmitted during self test sequence always begins with FF FE DO instead of FF FE 2F 4 Battery pack replacement CAUTION USE ONLY ORIGINAL AND APPROVED BATTERY PACK see C Battery replacement requirements ...

Page 67: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 605 FEB 01 2008 Figure 201 Battery Pack Disassembly Reassembly ...

Page 68: ...h expiration date of the new battery 2 Tick the box Battery change On the label supplied with the battery kit 3 Fill the field Battery Type with the P N of the new battery written on its label 4 Fill the field Battery Expiry Date with expiration of the new battery 5 Fill the field Inspection Date with today s date 6 Fill the field Next Control with the date of next mandatory control according to r...

Page 69: ...INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG KANNAD 406 AF COMPACT PAGE 607 FEB 01 2008 Figure 202 Recording of Maintenance Tasks ...

Page 70: ...e from the foam 2 Position the foam as to put the wire of the battery through the rectangular notch of the foam 3 Fold and stick the first leaf of the foam at the right of the notch on the right side of the battery pack 4 Stick the second leaf of the foam onto the front of the battery pack 5 Fold and stick the third part of the foam onto the left part of the battery pack 6 Fold and stick the fouth...

Page 71: ...the 4 securing screws and nuts with those supplied with the kit and torque to 1 newton meter 0 06 8 85 pound force inch 0 53 Remove the broken seal and replace it with the new seal supplied with the battery kit Check beacon watertightness Bring the water of a bath to a temperature of 50 C 5 C WARNING If an electrical heating source is used its power supply must be switched off while handling the b...

Page 72: ...s 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 saraviation 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 index en php Pages SAFETY AERONAUTIC ELT Only original and approved battery pack included in battery KIT BAT200 P N S1840501 0...

Page 73: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 74: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 75: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 76: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 77: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 78: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 79: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 80: ...eplacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has bee...

Page 81: ...replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp Type of inspection Periodic Battery change Repair Other Operations carried out Next recommended inspection date _ _ _ _ _ _ Next planned battery replacement mandatory date _ _ _ _ _ _ Date _ _ _ _ _ _ _ _ Service station Signature and stamp note complete P N of replaced components if battery pack has be...

Page 82: ...ocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp Identification protocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp ...

Page 83: ...ocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp Identification protocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp ...

Page 84: ...ocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp Identification protocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp ...

Page 85: ...ocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp Identification protocol TN ICAO AOD S N TEST Identification number Beacon identification 15 HEX ID Aircraft Tail Number Date _ _ _ _ _ _ _ _ Service station Signature and stamp ...

Page 86: ...SPECTION LOG KANNAD 406 AF COMPACT PAGE 624 FEB 01 2008 15 Pre delivery Inspection Log P N ________ __ AMDT _ S N 2615748 ____ CSN 3_____ DOM __ ____ Controlled By __ Next battery replacement before __ ____ Date __ __ __ Stamp FIT DECAL HERE ...

Page 87: ......

Page 88: ...DOC06006D Ref 0141922D 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 ...

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