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INITIAL INSTALLATION MANUAL

AF INTEGRA / AF-H INTEGRA

PAGE: 13

JUN 01/2011

IMPORTANT: tighten to a torque between 4 and 5 Newton x meter.

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 (ER), 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

.

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Содержание AF INTEGRA

Страница 1: ...D 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 ...

Страница 2: ...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 ...

Страница 3: ...andations 9 RTCA DO 204a Requirements 9 ELT location recommendations 10 Bracket installation procedure 10 Determine location and direction 10 Fix the mounting bracket 12 ELT installation procedure 13 Antenna Installation 15 Antenna Installation Recommendations 15 FAA Recommendations 15 RTCA DO 204 Recommendations for external antenna location 15 External Antenna Location 15 Antenna installation pr...

Страница 4: ...TS TOC PAGE 2 JUN 01 2011 121 5 MHz 31 Outline dimensions and weights 33 Wiring diagrams 48 Compatibility list for INTEGRA ELTs System 53 Mounting brackets 53 Remote control panels RCP 53 Outside buzzer 53 DIN 12 connector or programming dongles 53 External antennas 54 ...

Страница 5: ...esentation A System overview NOTE 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 1 a transmitter 2 a mounting bracket 3 a remote control panel RCP see note 1 page 2 4 a DIN 12 connector or programming dongle to connect the RCP 5 an approved external whip rod o...

Страница 6: ...nd 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 The ELT must be installed into one of the approved mounting brackets It may be installed on its...

Страница 7: ...et 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 1 RC100 KIT The RC100 remote control panel is connected to the ELT via a 3 wire cable equipped with a ...

Страница 8: ...ls 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 3 RC200 The RC200 or 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 d...

Страница 9: ...or 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 5 RC600 NVG The RC600 NVG is connected to the ELT via a 5 wire bundle equipped with a DIN 12 connector or optional programming dongle on the ELT side and a female 22 pin connector on the other side Figure 8 RC600 NVG Remote Control Panel ...

Страница 10: ...nection 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 ...

Страница 11: ... 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 ...

Страница 12: ...gistration 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 ...

Страница 13: ...at 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 th...

Страница 14: ...ever 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 INT...

Страница 15: ...TEGRA 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 helico...

Страница 16: ...stalled with the lower side pointing towards the front of the helicopter 2 Fix the mounting bracket Drill 4 holes Ø 6 mm in the aircraft structure according to Drilling mask Refer to Compact Mounting bracket S1840502 01 Outline dimensions and weight page 35 Inner holes 1 2 3 4 should be preferred or Refer to Compact Universal Mounting bracket S1840502 02 Outline dimensions and weight page 36 accor...

Страница 17: ...ansmitter 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 ER 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...

Страница 18: ...he 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 13 Installing the transmitter on the bracket ...

Страница 19: ... 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 interfere...

Страница 20: ...ure 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 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 Recommendati...

Страница 21: ...tline 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 conne...

Страница 22: ...t connectors Figure 15 Example of connection ELT to RCP NOTE 1 in order to easily remove the programming dongle when the RCP is connected to the ELT via a Programming Dongle P N S1820514 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 NOTE 2 The mounting of a stopping connector may be skipped by us...

Страница 23: ... 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 Ø 8 mm for the LED mounting 2 top of the panel Drill a hole Ø6 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 w...

Страница 24: ...r 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 ...

Страница 25: ... that can be either a standard DIN12 connector P N S1820514 03 or a connector with an integrated serial memory module called Programming Dongle P N S1820514 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 c...

Страница 26: ...for the switch 3b right of the panel Note the switch 3b is already soldered to a PCB 3a Drill 4 holes of Ø 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 PC...

Страница 27: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 23 JUN 01 2011 Figure 19 RC102 mounting diagram ...

Страница 28: ... 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 rivets 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 location belo...

Страница 29: ...4 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 from DIN 12 connector to the female 9 pin D SU...

Страница 30: ...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 programming dongle to be connected to the ELT or to the DIN 12 male...

Страница 31: ...eferred 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 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 RC...

Страница 32: ...ions 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 installatio...

Страница 33: ... 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 TEST on the Remote Control Panel ensure that the ELT switch is in position ARM Listen for the buzzer it operates during the whole Se...

Страница 34: ...switching ELT and RCP as described in the sequential procedure Figure 23 RCP LED operation with ELT switch in the ARM position Figure 23 RCP LED operation 3 1 LOW BATTERY VOLTAGE 3 2 LOW RF POWER 3 3 FAULTY VCO LOCKING FAULTY FREQUENCY 3 4 NO IDENTIFICATION PROGRAMMED 3 5 FAULTY VSWR EXT ANTENNA 3 6 GPS SERIAL LINK ELT internal check If self test fails contact the distributor as soon as possible U...

Страница 35: ...s with FF FE D0 whereas a programmed message begins with FF FE 2F Example of message programmed in ELT FF FE 2F 96 E3 AF 0F 0F 7F DF FF 62 60 B7 83 E0 F6 6C Example of same message decoded by Cospas Sarsat Decoder FF FE D0 96 E3 AF 0F 0F 7F DF FF 62 60 B7 83 E0 F6 6C 2 121 5 MHz This test must be carried out with a VHF receiver either with the aircraft VHF receiver of with a not on board VHF recei...

Страница 36: ...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 Cont...

Страница 37: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 33 JUN 01 2011 10 Outline dimensions and weights Figure 24 Outline Dimensions and weight with Compact Mounting Bracket ...

Страница 38: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 34 JUN 01 2011 Figure 25 Outline dimensions and weight with Universal Mouting Bracket ...

Страница 39: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 35 JUN 01 2011 Figure 26 Compact Mounting bracket S1840502 01 Outline dimensions and weight ...

Страница 40: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 36 JUN 01 2011 Figure 27 Compact Universal Mounting bracket S1840502 02 Outline dimensions and weight ...

Страница 41: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 37 JUN 01 2011 Figure 28 Outside buzzer Outline dimensions Figure 29 RC100 Outline dimensions ...

Страница 42: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 38 JUN 01 2011 Figure 30 RC102 Outline dimensions ...

Страница 43: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 39 JUN 01 2011 Figure 31 RC200 Outline Dimensions ...

Страница 44: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 40 JUN 01 2011 Figure 32 RC300 Outline Dimensions ...

Страница 45: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 41 JUN 01 2011 Figure 33 RC600 Outline dimensions ...

Страница 46: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 42 JUN 01 2011 Figure 34 AV 200 Outline dimensions and weight ...

Страница 47: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 43 JUN 01 2011 Figure 35 ANT300 Outline dimensions and weight ...

Страница 48: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 44 JUN 01 2011 Figure 36 AV 300 Outline dimensions and weight ...

Страница 49: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 45 JUN 01 2011 Figure 37 ANT500 Outline dimensions and weight ...

Страница 50: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 46 JUN 01 2011 Figure 38 ANT560 Outline dimensions and weight ...

Страница 51: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 47 JUN 01 2011 Figure 39 ANT650 Outline dimensions and weight ...

Страница 52: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 48 JUN 01 2011 11 Wiring diagrams Figure 40 RC100 Wiring diagram ...

Страница 53: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 49 JUN 01 2011 Figure 41 RC102 Wiring diagram ...

Страница 54: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 50 JUN 01 2011 Figure 42 RC200 Wiring diagram ...

Страница 55: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 51 JUN 01 2011 Figure 43 RC300 Wiring diagram ...

Страница 56: ...INITIAL INSTALLATION MANUAL AF INTEGRA AF H INTEGRA PAGE 52 JUN 01 2011 Figure 44 RC600 Wiring diagram ...

Страница 57: ...PACT UNIVERSAL MOUNTING BRACKET KIT S1840502 02 KANNAD Designation KANNAD Part Number RC100 KIT S1820513 03 RC102 KIT S1820513 21 RC200 S1820513 11 RC300 S1820513 09 RC300 NVG S1820513 10 RC600 NVG Y S1820513 12 RC600 NVG W S1820513 13 KANNAD Designation KANNAD Part Number OUTSIDE BUZZER KIT S1820515 06 KANNAD Designation KANNAD Part Number DIN 12 connector S1820514 03 Programming dongle S1820514 ...

Страница 58: ... 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 S65 8282 406 0124222 BLADE ANT560 DAYTON GRANGER ELT10 696 1 0145787 BLADE ANT650 CHELTON 2624 82 0124251 N A CHELTON 21 41 N A ...

Страница 59: ......

Страница 60: ...DOC09081B Ref 0146259B Manufactured by Z I des Cinq Chemins BP23 56520 GUIDEL FRANCE http www kannad com 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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