00. Initial Installation Manual AF INTEGRA.book
Contents
1. TC y N 1 sejeuosip H M dea SALON eUJ9 X3 2 ONINSWM 1X3 jJeuondo i 2 Q D V Xs TONIC 52 3ENUG XL INDC 1X3 ND 837206 Jezznq 100 N37Zng jeuondo sazzng jeuondo 37708 dow 837704 dow 31 dod 77 7 31 doa NOWNDD doa NOWO 424 NO 454 NO 494 13534 438 VO 13538 438 dO INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA 002024 fe JO j2euuoo Jojoeuuoo 2 2 6 NS d Oo S o Oo S Q N Q GE i 9 5 5 aviation 113 KANNAD PAGE 50 JUN 01 2011 Jezznq OMV V Jezzng jeuondo 5918108 p 55 SALON ND 31950 ONDT J9Zznq euJo ul 9 qeue XL 3NUC els pue rt dens ND 337708 INIT J9ZZnq epis nO 59 INDC jeuondo 100 N3ZZn8 NIC 437714 424 837714 dod gt T m O Q ul u 31 doa 31 doa NUAAUO d23 NOWO dod NO 494 AF INTEGRA AF H INTEGRA lt 2 lt 2 a lt o lt lt N dow lt x 13534 494 13534 404 dow 006524 Figure 43 RC300 Wiring diagram JOo joeuuoo 6 A NS d aviation 1132. PAGE 42 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 35 ANT300 Outline dimensions and weight Note all dimensions are in millimeters inches in brackets GASKET _ DIA 45 35 0 77 1 38 TH 2 0 08 3 ATTACHMENT HOLES DIA 5 5 0 22 CSK90 PAGE 43 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 36 AV 300 Outline dimensions and weight Note all dimensions are in milimeters inches in brackets Weight 255 g 0 56 15 87 0 625 DIA Connector hole 5 56 0 21 9 DIA 34 14 1 344 3 Mounting holes PAGE 44 JUN 01 2011 INITIAL INSTALLATION MANUAL NNAD AF INTEGRA AF H INTEGRA Figure 37 ANT500 Outline dimensions and weight Note all dimensions are in millimeters inches in brackets Weight 730 g 1 61 Ibs 3000 1 175 1 825 BNC 45 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 38 ANT560 Outline dimensions and weight 129 5 5 10 139 7 5 50 Note dimensions are in millimeters inches in brackets rss 1 4 6 1 52 18 57 1 2 25 38 1 1 5 31 7 1 25 Weight 544g 1 20 Ibs 152 4 6 213 3 8 4 PAGE 46 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 39 ANT650 Outline dimensions and weight Note all dimensions a
3. registration authority 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 Once 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 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 7
4. 56 220 22 5 0 89 PAGE 28 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 8 ELT Connection Connect the cable of the external antenna to the BNC connector of the front panel Connect the DIN12 connector of the Remote Control Panel cable to the DIN 12 socket of the front panel Set the 3 position switch of the front panel to ARM Figure 22 Installation controls and connectors e Perform the first power up procedure see below 9 First power up procedure Do not perform these tests without the antenna connected 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 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 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 in
5. A INITIAL INSTALLATION MANUAL e aviation AF INTEGRA AF H INTEGRA Figure 18 RC100 mounting diagram Anode Cathode Long pin Short pin Detail of led Locked position Locked position ARMED Momentary position RESET amp TEST SYS XS HHWEANASSS 22 6 235 1 38 26 1 02 Connect RCP to ELT Solder the DIN12 connector or Programming Dongle on the other side of the bundle Refer to Figure 40 RC100 Wiring diagram page 48 Outside buzzer installation and connection option Mount and install buzzer Refer to Section 7 Outside Buzzer Installation page 28 Connect the buzzer to the ELT Refer to Figure 40 RC100 Wiring diagram page 48 PAGE 20 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 2 RC102 RC102 RCP is supplied as a kit Refer to Figure 19 RC102 mounting diagram page 23 2 types of front plates may be installed Choose the appropriate front plate according to the aircrafts instrument panel The kit also includes 2 LEDs The white LED is a NVG LED Night Vision Goggles only used for military aircraft the red LED is a standard LED CAUTION use NVG LED only for military aircraft equipped for night vision googles Never install this LED in RCP for standard aircraft Connection of RC102 requires a 2 wire bundle A pin to pin wiring has to be provided by the installer with AWG24 wires Shielded wires recommend
6. ELT side Solder the wires to the DIN 12 connector or programming dongle to be connected to the ELT or to the DIN 12 male connector of RCP bundle if a Programming Dongle ASSY is used Refer to Figure 17 Programming Dongle ASSY On the RCP side Solder the wires to the female 22 pin socket according to wiring diagram Connect Ouside Lamp Horn Lamp test and Backlight optional outside buzzer is connected Mount and install the buzzer Refer to Section 7 Outside Buzzer Installation page 28 Connect the buzzer Refer to Figure 44 RC600 Wiring diagram page 52 Put heat shrinkable sleeves to protect the pins Connect the female 22 pin socket to the male 22 pin plug of RC600 PAGE 27 JUN 01 2011 A INITIAL INSTALLATION MANUAL lt aviation AF INTEGRA AF H INTEGRA 7 Outside Buzzer Installation Drill 3 x 3mm holes according to drilling mask Refer to Figure 28 Outside buzzer Outline dimensions Fix the mounting tray 1 with 3 M3 screws and nuts or with 3 rivets Install the buzzer 2 on the into the mounting tray and tighten plastic nut 3 maximum torque on plastic nut 6Nm Crimp the Fast On terminals 4 on the wires Wrap the Fast On terminals with heat shrinkable sleeve 5 25 mm Using clamps 6 fix the wires on the mounting tray Affixed the label 7 on the wires Figure 21 Buzzer installation AWG24 Wire CF24 lt w w
7. INTEGRA AF H INTEGRA Figure 27 Compact Universal Mounting bracket S1840502 02 Outline dimensions and weight Note all dimensions are in millimeters Typical weight in grams inches in brackets pounds in brackets with attaching parts 182 0 40 50 08 1 97 o a e F 4470 176 46 20 1 82 am uem lt iv 99 12 3 90 4 05 58 0 22 m m 7 S PAGE 36 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 28 Outside buzzer Outline dimensions Note all dimensions are in millimeters inches in brackets 44 1 73 CAUTION Dimensions not to scale 27 7 1 09 Figure 29 RC100 Outline dimensions 30 1 18 ELT KANNAD 06 5 0 26 PAGE 37 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 30 RC102 Outline dimensions 30 118 ELIT KANNAD Test FAIL Test OK LY ON eM 0 551 10901 93 12081 RC102 Front plate 1b CAUTION Dimensions not to scale PAGE 38 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 31 RC200 Outline Dimensions Note all dimensions are in millimeters Tolerance 0 2 mm 0 008 inches in brackets 33 1 3 43 1 69 FOR AVIATION EMERGENCY USE ONLY UNAUTHORIZED OPERATION PROHIBITED 2 Oo N S CONTROL PANEL 3
8. for details of approved part number of AF INTEGRA AF H INTEGRA system Refer to Section 12 Compatibility list for INTEGRA ELTs System page 53 AF INTEGRA AF H INTEGRA system is composed of a transmitter a mounting bracket a remote control panel RCP see note 1 2 a DIN 12 connector or programming dongle to connect the RCP an approved external whip rod or blade antenna Figure 1 ELT system description Antennas not to scale Coaxial cable lt A 2 3 or 4 wire bundle G 24 PAGE 1 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA The most effective external antenna configuration is on top of the fuselage aft of the wing or near the vertical stabilizer The ELT and mounting bracket should be mounted in the aircraft as close as the antenna as practicable with a coaxial cable towards the antenna as short as possible The remote control panel is installed in the cockpit and connected to the ELT with a 2 3 4 wire bundle not supplied according to the type of Remote Control Panel 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 fli ght use shall be readily accessible from the cockpit crew position The cockpit crew shall have an unobstructed view of visual indicator when in the normal seated position B Transmitter and bracket
9. inside the LED mounting 2 e Install the switch and PCB assembly 3b 3a with washers and nuts 3d locked position upwards Tighten nut Stuck the identification label 4 on the cable bundle near the PCB Front plate 1b Place the front panel 1b on to the instrument panel and use it as drilling mask or Trace the centers of the two holes according to drilling mask supplied Drill a hole 8 mm for the LED mounting 2 left of the panel Drill a hole 26 5 mm for the switch 3b right of the panel Note the switch 3b is already soldered to a PCB 3a Drill 4 holes of 3 mm for the screws used to fix the RCP Screw the front plate 1b onto the instrument panel Install the LED mounting 2 with washer 2a and nut 2b Tighten nut Connect the anode long pin of LED 2c to A of PCB 3a Connect the cathode short pin of LED 2c to C of PCB 3a Connect wires to K and M of PCB 3a Insert the LED into the LED stand 2d taking care the flat part of the LED be in front of the flat part of the LED stand Insert LED 2c fitted with LED stand 2d inside the LED mounting 2 Install the switch and PCB assembly 3b 3a with washers 3c and nuts 3d locked position upwards Tighten nut Stuck the identification label 4 on the cable bundle near the PCB PAGE 22 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 19 RC102 mounting diagram A
10. location below the instrument panel be sure the location meets the requirements established 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 the 2 screws 6 supplied torque 0 8 Nm PAGE 24 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 20 Installation of RC200 with mounting tray Connection Refer to Figure 42 RC200 Wiring diagram page 50 RC200 is an RCP without internal buzzer It can be connected to an optional outside buzzer and or to an external warning A 3 wire bundle is required to connect RC200 to the ELT If the optional outside buzzer and or external warning is installed a 4 wire bundle is required Fabricate a 3 or 4 wire bundle AWG 24 shielded preferred long enough to reach between the ELT installation location and the cockpit RCP location Slide heat shrinkable sleeves on both sides of each wire On the ELT side Solder the wires to the DIN12 connector supplied with the pack according to wiring diagram Put heat shrinkable sleeves to protect the pins On the RCP side Solder the wires fr
11. on the label affixed to the top of the ELT a Fixed wing aircraft with AF INTEGRA Refer to Figure 10 KANNAD AF INTEGRA axis of installation 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 2 Consequently the AF INTEGRA shall be mounted with the arrow of the Flight direction label pointed towards the front of the aircraft in any position parallel to the roll axis b Helicopters with AF INTEGRA Refer to Figure 10 KANNAD AF INTEGRA axis of installation AF INTEGRA may be installed on helicopter The ELT unit should be mounted with maximum tolerance of 2 with Flight direction arrow towards the front of the helicopter with the front face connectors pointing downwards at a 45 angle to the yaw axis in any position parallel to the 45 axis c Helicopters with AF H INTEGRA Refer to Figure 11 KANNAD AF H INTEGRA axis of installation IMPORTANT AF H INTEGRA is designed to be mounted on board helicopters only PAGE 11 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 11 KANNAD AF H INTEGRA axis of installation YAW Axis Upper side Front face lt Lower side ia Upper side Lower side i Front face connectors Direction of Flight Arrow The Direction of Flight arrow shall point towards the front or the bottom of
12. other side Figure 4 RC100 Remote Control Panel PAGE 3 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 2 RC102 KIT The RC102 remote control panel is connected to the ELT via a 2 wire cable equipped with a DIN 12 connector or optional programming dongle on the ELT side and directly connected to the RCP on the other side 2 types of front panels are supplied in the kit The appropriate front panel should be choosen according to the place available on the aircraft s instrument panel Note the optional outside buzzer is not available with this RCP Figure 5 RC102 Remote Control Panel EZ P d 3 200 RC200 RC200 NVG remote control panel is connected to the ELT via a 3 or 4 wire bundle equipped with a DIN 12 connector or optional programming dongle on the ELT side and a D SUB Female 9 pins connector on the other side Figure 6 RC200 Remote Control Panel PAGE 4 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 4 RC300 RC300 NVG The RC300 is connected to the ELT via a 4 wire bundle equipped with a DIN 12 connector or optional programming dongle on the ELT side and a D SUB 9 PTS Male connector on the other side Figure 7 RC300 Remote Control Panel A ON ARMED T STIRESET 5 RC600 NVG The RC600 is connected to the ELT via a 5 wire bundle equipped with a DIN 12 connector or optional programming dongle on
13. the ELT side and a female 22 pin connector on the other side Figure 8 RC600 NVG Remote Control Panel PAGE 5 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA D External antennas The external antenna can be either of whip rod or blade type according to aircraft speed Connection to the ELT will be carried out with a 50 Ohm coaxial cable ended with two male BNC connectors IMPORTANT NOTICE KANNAD recommends a cable with radio electric properties similar or better to those of a RG58 cable Note the 50 Ohm coaxial cable and the male BNC connectors are not supplied Figure 9 Whip rod and blade antennas Whip antenna type Rod antenna type Blade antenna type PAGE 6 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 3 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 Any change of ownership shall also be declared and registered with the local
14. the helicopter and not pointing 45 downwards f the AF H INTEGRA 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 AF H INTEGRA 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 of the helicopter 2 Fix the mounting bracket Drill 4 holes 6 mm in the aircraft structure according to Drilling mask Refer to Compact Mounting bracket 51840502 01 Outline dimensions and weight page 35 Inner holes 1 2 3 4 should be preferred or Refer to Compact Universal Mounting bracket 51840502 02 Outline dimensions and weight page 36 according to mounting bracket used If the attachement system is not solid enough to withstand a 100G load bracket weight x 100 on the bracket a reinforcement plate not supplied should be installed as shown Figure 12 Bracket installation in order to be compliant with the RTCA DO 182 recommendation Fixthe bracket with the 4 screws 8 washers and 4 nylstop nuts supplied PAGE 12 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA IMPORTANT tighten to a torque between 4 and 5 Newton x meter Screw 90 Washer small Mounting bracke Washer large Optional reinfor
15. use the appropriate outline drawings and drilling masks to determine the hole patern and drill size refer to the relevant antennae outline dimensions page 42 page 43 page 44 Fabricate a 50 Ohms coaxial cable long enough to reach between the ELT installation location and the antenna location IMPORTANT The use of a low attenuation coaxial cable is recommended The maximum permitted attenuation in the coaxial is 2db 400 MHz See Important notice External antennas page 6 Fit both ends of coaxial cable with a waterproof Male BNC connector not supplied reference RADIALL R141007 or equivalent Connect one Male BNC connector to the antenna Female BNC socket PAGE 17 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 6 RCP installation A RCP Installation Recommendations The RCP shall be installed in the cockpit The RCP shall be readily accessible from the pilot s normal seated position B RCP Installation Procedure The RCP must be connected to the ELT via a DIN 12 connector P N 51820514 03 or a Programming Dongle Refer to Section 12 Compatibility list for INTEGRA ELTs System page 53 on the ELT side and the relevant mating connector of the RCP on the RCP side except for RC100 and RC102 wires directly connected to the RCP without connectors Figure 15 Example of connection ELT to RCP RCP bundle DIN 12 RCP ELT or Programming Dongle Mating connector NOTE 1 in order to easi
16. 03 RC102 KIT 51820513 21 RC200 51820513 11 RC300 51820513 09 RC300 NVG 51820513 10 RC600 NVG Y 51820513 12 RC600 NVG W 51820513 13 C Outside buzzer KANNAD Designation KANNAD Part Number OUTSIDE BUZZER KIT 51820515 06 D DIN 12 connector or programming dongles KANNAD Designation KANNAD Part Number DIN 12 connector 51820514 03 Programming dongle 51820514 01 Programming A320 51820514 04 Programming dongle A330 A340 51820514 05 Programming dongle Assy 51820514 06 53 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA E External antennas KANNAD Designation Manufacturer KANNAD Part Number ANT300 CHELTON 1327 82 0124220 WHIP ANT AV200 RAMI AV 200 0146150 ROD ANT AV300 RAMI AV 300 0146151 BLADE ANT500 SENSOR SYSTEMS 0124222 565 8282 406 BLADE 560 DAYTON GRANGER 0145787 ELT10 696 1 BLADE ANT650 CHELTON 2624 82 0124251 N A CHELTON 21 41 N A PAGE 54 JUN 01 2011 Manufactured by CANNAD aviation 2 1 des Chemins BP23 56520 GUIDEL FRANCE http www kannad com T l Phone 33 0 2 97 02 49 49 Fax 33 0 2 97 65 00 20 A Company of the Orolia Group DOC09081B Ref 0146259B
17. 2 PAGE 9 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA B ELT location recommendations KANNAD provides additional safety functions in the INTEGRA ELTs such as built in GPS and integral antenna If the link towards the external antenna is defective the integral antenna protected by the high resistance housing of the ELT may help to establish a link towards the satellites COSPAS SARSAT system However KANNAD cannot control neither the environment of the ELT when a crash occurs nor a too important metallic structure around the ELT For these reasons KANNAD recommends to install the ELT in a location in such a way that the vertical extension of the integral antenna is exposed to a RF transparent window C Bracket installation procedure 1 Determine location and direction Figure 10 KANNAD AF INTEGRA axis of installation YAW Axis Front face connectors Roll Axis Front face connectors AON3OH3IN3 A9N39t3N 8WO1V201 2N3583W3 Direction of Flight Arrow Determine the location of the ELT onboard cem to paragraph A ELT and bracket installation recommendations page 9 The G Switch axis shall be directed to sense the primary crash pulse PAGE 10 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA along the longitudinal axis of the aircraft Reference to the G Switch is given by the arrow Flight direction
18. 283 or 301 817 4515 Failure to register re register as required every two years or to notify NOAA PAGE 7 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 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 information 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
19. 3 1 23 20 0 787 26 4 1 04 7 0 275 zt 0 197 Front View PER Side View 6 0 236 MOUNTING TRAY 26 4 1 04 CAUTION Dimensions not to scale PAGE 39 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 32 RC300 Outline Dimensions Note All dimensions are in millimeters inches in brackets 146 5 748 4 ON ARMED TEST RESET N e co 40 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 33 RC600 Outline dimensions Note All dimensions are in millimeters inches in brackets 136 3 0 15 5 366 0 006 1 499 0 0197 4 89 0 15 0 187 006 0 192 0 006 lt gt 0 146 0 5 5 748 0 0197 127 5 Max 33 1 299 7 6 0 5 62 2 2 44 0 08 0 3 0 019 34 8 1 37 max 44 8 1 1 764 0 0393 PAGE 41 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 34 AV 200 Outline dimensions and weight Note all dimensions are in milimeters inches in brackets Weight 85 g 0 19 Ibs 9609 13 0 515 2127 0 500 12 1 CY e Mounting Hole Mounting Hole option 1 option 2 Moisture seal Outside of aircraft Mounting hole through es aircraft skin aian Name plate 5 Lock washer Hex nut amp
20. ANNAD AF INTEGRA AF H INTEGRA 10 Outline dimensions and weights Figure 24 Outline Dimensions and weight with Compact Mounting Bracket 140 5 512 Weight in grams pounds in brackets AF INTEGRA 880 1 94 ga o NQ D c 2 E e AF H INTEGRA 885 1 95 86 4 3 40 RC inches in brackets 98 3 858 Note all dimensions are in millimeters Ant Arm Off On PAGE 33 JUN 01 2011 A INITIAL INSTALLATION MANUAL aviation AF INTEGRA AF H INTEGRA Figure 25 Outline dimensions and weight with Universal Mouting Bracket Weight in grams pounds in brackets S 5 o t gt 5 INTEGRA 905 1 99 AF H INTEGRA 910 2 00 RC inches in brackets Ant Arm Off On Note all dimensions are in millimeters v 99 PAGE 34 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Figure 26 Compact Mounting bracket S1840502 01 Outline dimensions and weight Note all dimensions are in millimeters Typical weight in grams inches in brackets pounds in brackets with attaching parts 157 0 35 0 653 64 8 2 55 29 1 14 20 _ 2 7 eo 2 801 98 3 858 35 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF
21. DOCO09081B Ref 0146259B x LE E o c 6 6 gt 4 2 2 i A Company of the Orolia Group INITIAL INSTALLATION MANUAL in GPS and Integral Antenna AF INTEGRA AF H INTEGRA With built Revision 01 1senbe uodn qVNNVX 01 pauinjas eq jjeus jueuinoop eui eiouueuun J q eouejdeooe JOU ay Aq pesn eq jou 128 uoieuuojui eu 121 pue QVNNVX 10 sseJdxe pesojosip eq 5 peurejuoo eu JOU JUBLUNDOP eui jeu sseJdxe AY uo si juauinoop Bguepyuoo pue pue 30 Kuedoad aui si 5141 Date of rev JUN 01 2011 First issue OCT 10 2010 Users are 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 orolia com Tel 33 0 2 97 02 49 00 e INITIAL INSTALLATION MANUAL NNAD AF INTEGRA AF H INTEGRA TABLE OF CONTENTS Introduction KANNAD INTEGRA System Presentation System overview Transmitter and bracket Remote Control Panels RCP RC100 KIT RC102 KIT RC300 RC300 NVG RC600 NVG External antennas Registration General Regist
22. ELT side the wires are soldered to a 12 pin plug that can be either a standard DIN12 connector P N 51820514 03 or a connector with an integrated serial memory module called Programming Dongle P N 51820514 01 Mount and install RCP Refer to Figure 18 RC100 mounting diagram NOTE Pins of LED pins of switch and resistor must be protected by heat shrinkable sleeves Place the front plate 1 on the instrument panel Trace the centers of the two holes according to drilling mask supplied Drill a hole 8 mm for the LED mounting 2 top of the panel Drill a hole 26 5 mm for the switch 3 bottom of the panel Tear off protection from self adhesive film Stick the front plate 1 on the instrument panel Install the LED mounting 2 with washer 2a and nut 2b Tighten nut Solder the resistor 4 to pin 1 of Switch 3 Connect the anode long pins of LED 5 to pin 2 of switch 3 Make a strap between pin 3 of switch 3 and resistor 4 Connect wires to pin 2 of switch 3 the resistor 4 and the cathode short pins of LED 5 Stuck the identification label 6 on the cable bundle near the switch Insert the LED into the LED stand 7 taking care the flat part of the LED be in front of the flat part of the LED stand Insert LED 5 fitted with LED stand 7 inside the LED mounting 2 Install the switch 3 with washer 3a and nut 3b locked position upwards Tighten nut PAGE 19 JUN 01 2011
23. It should be mounted away from projections such as a propeller tail surfaces or the shadow of large antennas It is the responsibility of the installation agency to determine the appropriate and adequate antenna installation Locate a position on the fuselage according to Section 2 RTCA DO 204 Recommendations for external antenna location page 15 A double plate may be necessary for the antenna to meet rigidity specifications in Section 2 RTCA DO 204 Recommendations for external antenna location page 15 A 9 Kilogram force 20 pound force applied in all direction should not cause an appreciable distorsion in the aircraft skin Each of the approved antennas requires a ground plane On fabric covered aircraft or aircraft with other types on nonmetallic skins a ground plane must be added This can be accomplished by providing a number of metal foil strips in a radial position from the antenna base and secured under the fabric or wood skin of the aircraft The length of each foil radial should be at least equal to the antenna length and width atleast 1 inch due to the diameter of the antenna The ground plane must be connected to the shield of the antenna connector PAGE 16 JUN 01 2011 A INITIAL INSTALLATION MANUAL lt aviation AF INTEGRA AF H INTEGRA See figure below Antenna Metal foil under fabric or wood skin Figure 14 Antenna ground plane for non metallic aircraft According to the antenna to be installed
24. KANNAD PAGE 51 JUN 01 2011 AF INTEGRA AF H INTEGRA lt 2 lt 2 a lt o lt lt aviation KANNAD Figure 44 RC600 Wiring diagram 1 YDY LHOM 2 847708 AGISLNO 012209 3015100 dWV1 1531 dWV1 NYOH 3415110 GND SISSVHD dWV1 30151 837718 424 Q31 828 NUNND3 424 NO 13534 ddd Ir 00954 Jezznq OMY V uoneouisse o S310N 82 ade A IA 1 zzng episino J9zznq qeu ND 3 ND 1 zznq 1 3 FINO jeuondo 3 XL psa XS 319ND 82 52 4 Xa JND UJOH G9 sz pisinO JND ONINNVADDYd 437708 424 137 doa NOWNOD 454 NO dod 13534 424 119 JO utd zz dou 113 Ld PAGE 52 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 12 Compatibility list for INTEGRA ELTs System A Mounting brackets KANNAD Designation KANNAD Part Number COMPACT MOUNTING BRACKET KIT S1840502 01 COMPACT UNIVERSAL MOUNTING BRACKET KIT 51840502 02 B Remote control panels RCP KANNAD Designation KANNAD Part Number RC100 KIT 51820513
25. RA AF H INTEGRA C 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 should be carried out with a COSPAS SARSAT decoder Note 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 self test Press RESET and TEST on the RCP or 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 D0 whereas a programmed message begins with FF FE 2F Example of message programmed in ELT FF FE 2F 96 AF OF 7F DF FF 62 60 B7 83 F6 6C Example of same message decoded by Cospas Sarsat Decoder FF FE DO 96 AF OF 7F DF FF 62 60 B7 83 EO F6 6C 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
26. The ELT must be installed into one of the approved mounting brackets It may be installed on its standard mounting bracket or on a Universal Mounting Bracket to re use existing drilling for retrofit Refer to Section 12 Compatibility list for INTEGRA ELTs System page 53 for Part Numbers of approved mounting brackets The bracket installed near the tail is designed to fix the ELT with a Velcro amp strap This enables quick removal of the ELT for maintenance or exchange Figure 2 INTEGRA ELT with Mounting Bracket Velcro strap Bracket PAGE 2 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA C Remote Control Panels RCP Refer to Section 12 Compatibility list for INTEGRA ELTs System page 53 for Part Numbers of approved RCPs The RCP must be installed in the cockpit to monitor and control the ELT status It must be connected via a 2 3 or 4 wire bundle to the DIN 12 socket of the ELT 2 3 4 wire bundle is not supplied Note An optional outside buzzer assembly can be connected to the ELT RCP It gives an audio indication of emergency location transmitter ELT activation It is supplied with a mounting tray to install the buz zer on the aircraft Figure 3 Outside buzzer 3 1 RC100 KIT The RC100 remote control panel is connected to the ELT via a 3 wire cable equipped with a DIN 12 connector or optional programming dongle on the ELT side and directly connected to the RCP on the
27. ble Methods Techniques and Practices Aircraft Alterations specifically Chapters 1 3 11 and 13 2 RTCA DO 204 Recommendations for external antenna location ELT antennas should be located away from other antennas to avoid disruption of antenna radiation patterns Idealistically for the 121 5 MHz ELT antenna 2 5 meter separation is sufficient separation from VHF communications and navigation receiving antennas to minimize unwanted interferences ELT antennas should be 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 shall be such as to minimize radio frequency interference and radiation pattern distorsion of either antenna Coaxial cable connecting the ELT antenna installation should not cross the aircraft production breaks and should have vibrations proof RF connectors on each end The coaxial connecting the ELT transmitter to the external Antenna should be secured to the aircraft structure and when the coaxial cable is installed and the connectors are mated each end should be have some slack 3 External Antenna Location EUROCAE ED62A 6 1 10 2 most effective a
28. cement Nylstop nut plate not supplied Figure 12 Bracket installation D ELT installation procedure 1 Mount the transmitter on the bracket For AF INTEGRA or AF INTEGRA ER with Flight Direction Arrow of the ELT pointed towards the front of the aircraft according to Figure 10 KANNAD AF INTEGRA axis of installation page 10 For AF H INTEGRA or AF H INTEGRA with Flight Direction Arrow of the ELT pointed towards the front or downwards the helicopter according to Figure 11 KANNAD AF H INTEGRA axis of installation page 12 PAGE 13 JUN 01 2011 INITIAL INSTALLATION MANUAL NNAD AF INTEGRA AF H INTEGRA 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 Fasten the self stripping strap tightly Figure 13 Installing the transmitter on the bracket PAGE 14 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 5 Antenna installation Use only whip rod or blade approved antennas A Antenna Installation Recommendations 1 FAA Recommendations Installation must be made by qualified personnel in accordance with FAA regulations Duplicating a previous installation may not be acceptable Methods for installing antenna are outlined in AC43 13 12 refer to FAA Advisory Circular 43 13 2B Accepta
29. dicates that the system is operational and that error conditions were found A series of short flashes indicates the test has failed PAGE 29 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Remark The number of flashes gives an indication of the faulty parameter detected during the self test 3 1 LOW BATTERY VOLTAGE 3 2 LOW RF POWER 3 3 FAULTY VCO LOCKING FAULTY FREQUENCY 3 4 NO IDENTIFICATION PROGRAMMED 345 FAULTY VSWR EXT ANTENNA 346 GPS SERIAL LINK ELT internal check If self test fails contact the distributor as soon as possible Unless a waver is granted flight should be cancelled B RCP operational tests Check correct operation of RCP LED annunciator by switching ELT and RCP as described in the sequential procedure Figure i 23 RCP LED operation with ELT switch in the ARM position START TEST E EST RESE then ARMED Self test Wait end of self test 15 sec max a ELT amp RCP visual indicators flashing ELT buzzer modulated activation 3 ARMED ELT continues to transmit ELT amp RCP visual indicators flashing ELT buzzer modulated activation EST RESE 2 at least 1 sec then ARMED ELT transmission stops ELT amp RCP visual indicators are OFF ELT buzzer stops END OF TEST Figure 23 RCP LED operation PAGE 30 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEG
30. ed The wires are soldered to a PCB installed on the switch This operation can be carried out before installation On the ELT side the wires are soldered to a 12 pin plug that can be either a standard DIN12 connector P N 51820514 03 or a connector with an integrated serial memory module called Programming Dongle P N 51820514 01 Mount and install RCP Refer to Figure 19 RC102 mounting diagram page 23 NOTE Pins of LED must be protected by heat shrinkable sleeves Front plate 1a Place the front plate 1a on the instrument panel and use it as drilling mask or Trace the centers of the two holes according to drilling mask supplied Drill a hole 8 mm for the LED mounting 2 top of the panel Drill a hole 26 5 mm for the switch 3b bottom of the panel Note the switch 3b is already soldered to a PCB 3a Tear off protection of front plate 1a from self adhesive film Stick the front plate 1a onto the instrument panel Install the LED mounting 2 with washer 2a and nut 2b Tighten nut Connect the anode long pin of LED 2c to A of PCB 3a Connect the cathode short pin of LED 2c to C of PCB 3a Connect wires to K and M of PCB 3a Insert the LED into the LED stand 2d taking care the flat part of the LED be in front of the flat part of the LED stand PAGE 21 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Insert LED 2c fitted with LED stand 2d
31. either with the aircraft VHF receiver of with a not on board VHF receiver IMPORTANT Aircraft VHF receiver may be used only if 406 MHz test was carried out with a Cospas Sarsat 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 e Start transmission either on ELT ON position oron the RCP ON position the ELT shall be in ARM position Only 2 sweep tones are heard after 5 seconds then the 121 5 MHz stops PAGE 31 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Stop transmission either on ELT OFF or ARM position or on the Remote Control Panel press TEST and RESET the ELT shall be in ARM position 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 the satellite system 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 or manually by Remote Control Panel Note switching to ON directly on the ELT front panel will also activate the ELT PAGE 32 JUN 01 2011 INITIAL INSTALLATION MANUAL
32. ly remove the programming dongle when the RCP is connected to the ELT via a Programming Dongle P N 51820514 01 it is recommended to fit its cable with a stopping connector as close as possible to it see figure below Figure 16 Bundle with stopping connector Stopping connector Female connector Male connector ELT RCP Programming Short cable Long cable dongle NOTE 2 The mounting of a stopping connector may be skipped by using our pre wired Programming Dongle ASSY P N 8182051 4 06 This dongle is fitted with the Programming Dongle 51820514 01 on the ELT side and a female DIN 12 connector on the RCP side In this case a RCP bundle must be fabricated using a male DIN 12 connector reference P N 51820514 03 or BINDER 680 1 09 0329 00 12 and the relevant mating connector of the RCP Figure 17 Programming Dongle ASSY Male Din12 Programming dongle assy RCP bundle 15 T e PAGE 18 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 1 RC100 RC100 RCP is supplied as a kit Refer to Figure 18 RC100 mounting diagram Connection of RC100 requires a 3 wire bundle or 5 wire bundle if an outside buzzer is connected A pin to pin wiring has to be provided by the installer with AWG24 wires Shielded wires are recommended The wires are soldered to the switch pins a resistor and LED pins This operation can be carried out before installation On the
33. node Cathode Long pin Short pin Detail of led Instrument panel x1 Heat shrinkable sleeves not supplied Locked position ocked position ARMED Momentary position RESET amp TEST 08 0 32 drilling 06 5 0 26 drilling CO FAL mrstT amp TESTCO Front plate PAGE 23 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA Connect RCP to ELT Solder the DIN12 connector or Programming Dongle on the other side of the bundle pins K and M Refer to Figure 41 RC102 Wiring diagram page 49 Stuck the CAUTION label on the cable bundle close to the DIN12 connector 3 RC200 The RC200 RCP is designed to be installed either on the instrument panel with 4 screws rivets bush recommended not supplied or below the instrument panel with a special mounting tray supplied Installation on the instrument panel Determine RC200 location on the instrument panel Make a cutout on the instrument panel according to the Drilling mask Refer to RC200 Outline Dimensions page 39 Mark the 4 holes needed for the RC200 using the drilling mask or the RC200 as a guide Drill the 4 marked holes diameter depending on rivets bush used Install the RC200 by fitting it into the cutout Secure the RC200 4 bush recommended Note Rivets bush are not supplied Installation below the instrument panel Refer to Figure 20 Installation of RC200 with mounting tray Determine RC200
34. ntenna configuration for typical high wing and low wing aircraft is an external antenna on top of the fuselage and aft of the wing high wing or near the vertical stabilizer low wing Both ELT antennas should be located away from other antennas to avoid disruption PAGE 15 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA of antenna radiation patterns Detuning of the 121 5 MHz antenna may be required avoid the effects of radiated inter modulation products which may be possible from non operating 121 5 MHz ELTs exposed to high levels of RF energy Idealistically for the 121 5 MHz ELT antenna 2 5 meter separation is sufficient separation from VHF communications and navigation receiving antennas to minimize unwanted interference The 406 MHz ELT antenna should be positioned at least 0 8 m from VHF communications and navigation receiving antennas to minimize interference External antennas which have been shown to be compatible with particular ELT will either be part of the ETSO TSO d ELT or will be identified in the ELT manufacturer s installation instructions Recommended methods for installing antenna are outlined in FAA AC 43 13 2B The Antenna should be mounted as close to the respective ELT as practicable B Antenna installation procedure 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
35. om DIN 12 connector to the female 9 pin D SUB connector according to wiring diagram Put heat shrinkable sleeves to protect the pins Outside buzzer installation and connection option Mount and install buzzer Refer to Section 7 Outside Buzzer Installation page 28 Connect the outside buzzer Refer to Figure 42 RC200 Wiring diagram page 50 PAGE 25 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA External warning installation and connection option Refer to Figure 42 RC200 Wiring diagram page 50 Connect the female 9 pin D SUB connector to the male 9 pin D SUB plug of the RC200 4 RC300 RC300 NVG The RC300 RCP is designed to be installed in a standard rack of an aircraft cockpit As compliant with NF L 65 211 standard no drilling is necessary to install this RCP The precise location of RC300 is to be determined according to aircraft manufacturer instruction A male 9 pin D SUB connector reference AMPHENOL 17DE09PTZ or equivalent must be used as mating connector to connect the bundle to the RCP connector Connection with DIN 12 connector or Programming dongle Refer to Figure 43 RC300 Wiring diagram page 51 Fabricate a 4 wire bundle AWG 24 shielded preferred long enough to reach between the ELT installation location and the cockpit panel RCP location Slide heat shrinkable sleeves on both sides of each wire On the ELT side Solder the wires to the DIN 12 connector or
36. programming dongle to be connected to the ELT or to the DIN 12 male connector of RCP bundle if a Programming Dongle ASSY is used Refer to Figure 17 Programming Dongle ASSY On the ROP side Solder the wires to the male 9 pin D SUB connector according to wiring diagram optional outside buzzer is connected Mount and install the buzzer Refer to Section 7 Outside Buzzer Installation page 28 Connect the buzzer Refer to Figure 43 RC300 Wiring diagram page 51 Put heat shrinkable sleeves to protect the pins Connect the male 9 pin D SUB connector to the female 9 pin D SUB plug of RC300 PAGE 26 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 5 RC600 NVG The RC600 NVG RCP is designed to be installed in a standard rack of a military helicopter cockpit As compliant with NF L 65 211 standard no drilling is necessary to install this RCP The precise location of RC600 is to be determined according to aircraft manufacturer instruction A female 22 pin socket reference D38999 26JC35SA must be used as mating connector to connect the bundle to the RCP connector Connection with DIN 12 connector or Programming dongle Refer to Figure 44 RC600 Wiring diagram page 52 Fabricate a 4 wire bundle AWG 24 shielded preferred long enough to reach between the ELT installation location and the cockpit panel RCP location Slide heat shrinkable sleeves on both sides of each wire On the
37. ration in USA Registration in Canada ELT Installation ELT and bracket installation recommendations FAA Recommendations TSO C126a Section 5 b Application Data Requirements RTCA DO 182 Recommandations RTCA DO 204a Requirements ELT location recommendations Bracket installation procedure Determine location and direction Fix the mounting bracket ELT installation procedure Antenna Installation Antenna Installation Recommendations FAA Recommendations RTCA DO 204 Recommendations for external antenna location External Antenna Location Antenna installation procedure RCP installation RCP Installation Recommendations RCP Installation Procedure RC600 NVG Outside Buzzer Installation ELT Connection First power up procedure ELT operational tests RCP operational tests 406 and 121 5 MHz transmission test TOC PAGE 1 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA TABLE OF CONTENTS 121 5 MHz Outline dimensions and weights Wiring diagrams Compatibility list for INTEGRA ELTs System Mounting brackets Remote control panels RCP Outside buzzer DIN 12 connector or programming dongles External antennas TOC PAGE 2 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 1 Introduction The instructions in this manual provide the information necessary for the initial installation of AF INTEGRA AF H INTEGRA ELT system 2 KANNAD INTEGRA System Presentation A System overview NOTE
38. re in millimeters inches in brackets Weight 540 g 1 19 Ibs 6 HOLES 152 4 6 DIA 5 6 0 22 DIA 9 9 0 39 76 2 CSK100 41 28 9 RING DIA 24x2 0 94 x0 08 270 1 10 63 122 3 4817 8 5 BNC CONNECTOR PAGE 47 JUN 01 2011 AF INTEGRA AF H INTEGRA lt 2 lt 2 a lt o lt lt aviation KANNAD 11 Wiring diagrams Figure 40 RC100 Wiring diagram 43228 5110 ade Jezzng Jezzng 9JI OMY V sejeJosip p uoneoyissej o JIAA SALON Syesul JO fe YO 5 d 2 Jojeuuoo ZL NIG NS 999 de3W JNO XL XS 52 31980 NOC 437708 dod NO ddd 31 494 NOWNDD dow 13538 494 VYSALNI PAGE 48 JUN 01 2011 AF INTEGRA AF H INTEGRA lt 2 lt 2 a lt o lt lt aviation KANNAD Figure 41 RC102 Wiring diagram 9JI NV y sejeuosip 5 AIM SALON sp sul JO ZL NIG 9 gt m O Q H OND 31950 de3W 31DND XL 3TDN G XS INOC 52 N 837704 404 NONWO NU dou 31 dod NUAADO 454 13938 494 113 49 01 2011 Jezznq episjnQ BuHIAA
39. 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 Additional information and registration forms can be found on the Canadian NSS website at http www nss gc ca site cospas sarsat INTRO e asp PAGE 8 JUN 01 2011 INITIAL INSTALLATION MANUAL ANNAD AF INTEGRA AF H INTEGRA 4 ELT installation A ELT and bracket installation recommendations The ELT shall not be installed within 30cm 1 ft of a compass or flux gate The distance between ELT and antenna shall be determined so that according to the coaxial cable choosen The ELT front panel should be easily accessible to connect the external antenna and the remote control panel device and to check the ELT good operation controls and lights 1 FAA Recommendations Installation must be made by qualified personnel in accordance with FAA regulations Duplicating a previous installation may not be acceptable Refer to FAA Advisory Circular 43 13 2B Acceptable Methods Techniques and Practices Aircraft Alterations specifically Chapters 1 2 11 and 13 2 TSO C126a Section 5 b Application Da
40. ta Requirements The conditions and tests for TSO approval of this article are minimum performance standards Those installing this article on or in a specific type or class of aircraft must 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 manner that the attachment system can support a 100g load in the plus and minus directions of the three principal axes of the aircraft 4 RTCA DO 204a Requirements ELT unit shall be mounted to primary aircraft load carrying structures such as trusses bulkheads longerons spars or floor beams not aircraft skin or a structure that meets the requirements of the following test The mounts shall have a maximum static local deflection no greater than 2 5 mm when a force of 450 Newtons 100 Ibf 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 m or more than 1 0 m from the mounting location Typical approaches for adding shelf and rail platform mounting provisions to aircraft structure as shown an FAA Advisory circular 43 13 2 Chapter
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