Kannad 406 AP-H User manual

DOC06330E
Ref. 0143020E
TP PAGE : 1
Date of rev. JUL 24/2013
Revision 04
First issue: OCT 18/2006
Emergency Locator Transmitter
Orolia S.A.S. - A Company of the Orolia Group
INSTALLATION MANUAL
OPERATION MANUAL
KANNAD 406 AP-H
P/N : S1820502-04 KANNAD 406 AP-H transmitter
P/N : S1820511-01 Mounting bracket, 1 strap
P/N : 0124206 ANT100, auxiliary antenna
© Orolia S.A.S.: This document is the property of Orolia S.A.S. and contains proprietary and confidential information.
The document is loaned on the express condition that neither the document itself nor the information contained therein shall be disclosed without the express consent of Orolia S.A.S. and that the information

Users are kindly requested to notify Orolia S.A.S of any discrepancy,
omission or error found in this manual.
Please report to our customer support:
E-mail: [e-mail]
Tel.: [phone]

INSTALLATION MANUAL OPERATION MANUAL
KANNAD 406 AP-H
RECORD OF REVISIONS
ROR PAGE: 1
JUL 24/2013
REV. Nb REVISION DATE INSERTION DATE BY
00 OCT 18/2006 OCT 18/2006 J. S.
01 FEB 13/2008 FEB 13/2008 J. S.
02 SEP 12/2008 SEP 12/2008 J. S.
03 APR 30/2010 APR 30/2010 J. S.
04 JUL 24/2013 JUL 24/2013 J. S.

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SUBJECT PAGE DATE
Title Page
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Record of Revisions
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List of Effective Pages
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Table of Contents
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Introduction
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System Overview
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System Functional Description and Operation

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Check
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Troubleshooting
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INSTALLATION MANUAL OPERATION MANUAL
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TABLE OF CONTENTS
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INTRODUCTION ..................................................................................... 1
SYSTEM OVERVIEW ............................................................................. 1
COSPAS-SARSAT System ................................................................... 1
Description .............................................................................................................1
World coverage with the COSPAS-SARSAT system ............................................2
Environmental improvements of ELTs ................................................................... 2
G-Switch (shock detectors) .................................................................................... 2
KANNAD 406 AP-H Presentation ......................................................... 3
LINE REPLACEABLE UNITS ............................................................... 4
Transmitter ............................................................................................................ 4
Bracket ..................................................................................................................4
Remote Control Panel ...........................................................................................4
External antenna ................................................................................................... 4
Design features ..................................................................................... 5
Compatibility list .................................................................................... 6
Remote control panels (RCP) ................................................................................ 6
DIN-12 connector or programming dongles ...........................................................6
ELT-NAV System Interface .................................................................................... 6
External antennas.................................................................................................. 7
SYSTEM FUNCTIONAL DESCRIPTION AND OPERATION ............ 101
Transmitter ........................................................................................ 101
Controls ............................................................................................. 102
Working mode information ................................................................ 103
Off ...................................................................................................................... 103
Self-Test ............................................................................................................ 103
Armed ................................................................................................................ 104
On ...................................................................................................................... 104
Autonomy .......................................................................................... 105
Electrical characteristics .................................................................... 106
Electrical interface ............................................................................................. 106
Technical Specifications .................................................................... 107
Activation ........................................................................................... 108
Standby mode for automatic activation .............................................................. 108
Manual activation as fixed ELT .......................................................................... 108
Manual activation as survival ELT ..................................................................... 108
Reset ................................................................................................. 109
Manual reset ...................................................................................................... 109
Reset with Remote Control Panel ...................................................................... 109
Self-Test ............................................................................................ 109
INSTALLATION / REMOVAL ............................................................. 201
Registration and Programming ......................................................... 201
Pin programming option ....................................................................................201

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ELT Installation ................................................................................. 203
Installation recommandations ............................................................................ 203
FAA Recommendations .................................................................................. 203
TSO C126a Section 5 b. Application Data Requirements .............................. 203
RTCA DO-182 Recommandations .................................................................. 203
RTCA DO-204a Requirements ....................................................................... 203
Bracket installation ............................................................................................ 204
Transmitter and auxiliary antenna installation ................................................... 206
Antenna Installation .......................................................................... 208
Antenna Installation Recommendations ............................................................ 208
FAA Recommendations .................................................................................. 208
RTCA DO-204 Requirements for ELT location ............................................... 208
Antenna installation procedure .......................................................................... 208
First power up ................................................................................... 210
Removal ............................................................................................ 210
CHECK ............................................................................................... 301
Self-test ............................................................................................. 301
Periodicity .......................................................................................................... 301
Self-test procedure ............................................................................................ 301
ELT operational tests ........................................................................ 302
Installation without programming dongle ........................................................... 302
Installation with Programming Dongle ............................................................... 302
RCP operational tests ....................................................................... 303
406 and 121.5 MHz transmission test ............................................... 304
ELT-Antenna link ............................................................................................... 304
406 MHz ............................................................................................................ 304
121.5 MHz ......................................................................................................... 304
TROUBLESHOOTING ........................................................................ 401
General ............................................................................................. 401
Faults on Self-test ............................................................................. 401
Visual indicator .................................................................................................. 401
3+1 flashes ..................................................................................................... 401
3+2 flashes ..................................................................................................... 401
3+3 flashes ..................................................................................................... 401
3+4 flashes ..................................................................................................... 401
Other faults detected ......................................................................... 401
Buzzer ............................................................................................................... 401
Buzzer does not operate ................................................................................. 401
Buzzer operates permanently when ELT in ARM mode ................................. 401
SCHEMATICS & DIAGRAMS ............................................................ 501
Outline Dimensions ........................................................................... 501
Drilling Mask ..................................................................................... 502

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Wiring ................................................................................................ 503
ANT AV200, outline dimensions and drilling mask ........................... 504
ANT AV300, outline dimensions and drilling mask ........................... 505
ANT300, outline dimensions and drilling mask ................................. 506
ANT 410, outline dimensions and drilling mask ................................ 507
SERVICING ........................................................................................ 601
Maintenance Schedule ..................................................................... 601
Periodic inspection ............................................................................................ 601
Every 6 years .................................................................................................... 601
Battery replacement .......................................................................................... 602

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INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AP-H
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INTRODUCTION
The instructions in this manual provide the information necessary for the
installation and the operation of KANNAD 406 AP-H ELT.
Servicinginstructions(Referto SERVICING page601) arenormallyperformed
by shop personnel.
For servicing and maintenance instructions, refer to relevant CMM.
For regulatory requirements, please consult your national aviation authority.

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SYSTEM OVERVIEW
1. COSPAS-SARSAT System
A. Description
Launched in the early eighties by the four founder countries (Canada, France,
Russia, USA), the COSPAS-SARSAT system provides satellite aid to search
and rescue (SAR) operations for maritime, aeronautical and terrestrial vehicles
anywhere in the world.
It uses distress 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 (Emergency Position Indicating Radio Beacon) for maritime
applications.
• ELT (Emergency Locator Transmitter) for aeronautical applications.
• PLB (Personal Locator Beacon) for land expeditions.
Figure 1: COSPAS-SARSAT System

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B. World coverage with the COSPAS-SARSAT system
The major improvement is the use of the COSPAS-SARSAT system for
processing aeronautical emergencies.
The difference with the 121.5 / 243 MHz is that the 406 MHz transmission
carries digital data which enable the identification of the aircraft in distress and
facilitate SAR operation (type of the aircraft, number of passengers, type of
emergency).
The 406 MHz message is transmitted to the COSPAS-SARSAT satellites. This
message is downloaded to one of the 64 ground stations (44 LEOLUTs and 20
GEOLUTS).
The aircraft is located by Doppler effect by the LEO satellites with a precision
better than 2 NM (4 km) at any point of the earth.
C. Environmental improvements of ELTs
The certification of an ELT includes a range of severe mechanical tests:
• resistance to flame;
• impact and crush tests;
• resistance to 100 G and 500 G shocks;
• watertightness;
• antideflagration;
• extreme temperatures (-20°C to 55°C for more than 48 hours).
D. G-Switch (shock detectors)
The shock detectors equipping old automatic ELTs are the cause of a large
number of false alarms. Major work has consisted in studying aircraft crashes
(study made by the " Crash Research Institute ") and evaluating the
acceleration amplitudes involved. As a consequence, G-Switch specifications
have been modified to optimize the accuracy of the crash detection.

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2. KANNAD 406 AP-H Presentation
The KANNAD 406 AP-H belongs to the AP type of ELTs which are intended to
be rigdly attached to the aircraft before the crash, but readily removable from
the aircraft after a crash.
The KANNAD 406 AP-H is designed to be installed on helicopters only.
The KANNAD 406 AP-H is composed of:
1. a transmitter;
2. a mounting bracket;
3. a remote control panel (mandatory if ELT controls are not available from
the pilot’s position, refer to RTCA/DO-183, RTCA/DO-204, EUROCAE
ED-62);
4. an outside antenna;
5. a "Programming Dongle" for pin-programming function (option);
6. CS144 Interface Module (option);
7. an auxiliary antenna (for use as a survival beacon).
The transmitter, bracket, Programming Dongle and CS144 Interface Module
are installed in the aircraft near the tail. The outside antenna is mounted on the
fuselage near the tail. The remote control panel is installed in the cockpit and
connected to the ELT with a 4 or 5 wire bundle.
Figure 2: ELT system description
. Power Supply
. Nav System
1
2
465
2
3
System with optional CS144
1
2
3
5
4BNC Connector
4 wire bundle
AWG 24
Coaxial cable
Max cable loss = 1 dB
(i.e 2 mtrs with RG 58)
System without optional CS144 7
7

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3. LINE REPLACEABLE UNITS
A. Transmitter
The KANNAD 406 AP-H is an ELT designed to be installed on board
helicopters to transmit a distress signal on 3 frequencies:
• 406 MHz (COSPAS-SARSAT frequency) for precise pinpointing and
identification of the aircraft in distress.
• 121.5 and 243 MHz used for homing in the final stages of the rescue
operations.
It is certified as an Automatic Portable (AP) ELT and works with a three
frequency outside antenna when installed on board the aircraft or with a small
whip antenna (auxiliary antenna) when used as a survival ELT.
B. Bracket
The bracket installed near the tail is designed to fix the ELT with a Velcro®
strap. This enables quick removal of the ELT for maintenance or exchange.
C. Remote Control Panel
A remote control panel can be supplied for installation in the cockpit in order to
enable the pilot to monitor and control the ELT status.
The following controls are to be found on the panel:
• 3-position switch (ON, ARMED, RESET&TEST);
• red or amber visual indicator;
• beeper (on certain versions).
The remote control panel is connected to the ELT via a 4 or 5-wire cable
equipped with a "Programming Dongle" or a DIN 12 connector on the ELT side
and the connector corresponding to the Remote Control Panel version on the
other side.
D. External antenna
Theexternalantenna,alsoinstallednearthetail, canbeeither rodorblade type
according to aircraft speed.
Connection to the ELT will be carried out with a 50 Ohm coaxial cable (RG58
for example) ended with a BNC connector.
IMPORTANT NOTICE: Orolia S.A.S. recommends a cable with radio
electric properties similar or better to those of a RG58 cable.

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4. Design features
The KANNAD 406 AP-H is made of moulded plastic with excellent mechanical
resistance (ASA/PC, light yellow colour).
The housing is designed with no sharp edges.
Figure 3: KANNAD 406 AP-H with mounting bracket
ANT
ARM OFF ON RC

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5. Compatibility list
A. Remote control panels (RCP)
B. DIN-12 connector or programming dongles
C. ELT-NAV System Interface
Orolia Designation Orolia Part Number
RC100 KIT S1820513-03
RC150 KIT S1820513-07
RC200 S1820513-11
RC200-NVG S1820513-14
RC300 S1820513-09
RC400 S1820513-05
RC500-320 S1820513-02
RC600 NVG (Y) S1820513-12
RC600 NVG (W) S1820513-13
RC800 S1820513-15
RC810 S1820513-23
Orolia Designation Orolia Part Number
DIN-12 connector S1820514-03
Programming dongle S1820514-01
Programming dongle A320 S1820514-04
Programming dongle A330-340 S1820514-05
Programming dongle Assy S1820514-06
Orolia Designation Orolia Part Number
CS144-RS S1825502-01
CS144-A S1825502-02
Connecting cable for CS144-RS or CS144-A S1825502-03