Kannad 406 AF-COMPACT User manual

Emergency Locator Transmitters
DOC06006D
Ref. 0141922D
TP PAGE : 1
Date of rev. FEB 01/2008
Revision 03
First issue: FEB 01/2007
INSTALLATION MANUAL
OPERATION MANUAL
INSPECTION LOG
KANNAD 406 AF-COMPACT
P/N : S1840501-02 Pack ELT KANNAD AF-COMPACT
© KANNAD: 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 shall be returned immediately to KANNAD upon request.


INSTALLATION MANUAL OPERATION MANUAL INSPECTION 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.

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KANNAD 406 AF-COMPACT
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SUBJECT PAGE DATE
Title Page
TP 1 FEB 01/2008
Record of Revisions
ROR 1 FEB 01/2008
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
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System Functional Description and Operation
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Check
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Troubleshooting
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Schematics and Diagrams 501 FEB 01/2008
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Servicing
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TABLE OF CONTENTS
TOC PAGE: 1
FEB 01/2008
INTRODUCTION ..................................................................................... 1
WARRANTY ........................................................................................... 2
Scope .................................................................................................... 2
Exclusion ............................................................................................... 2
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 ELTs Presentation .......................................................... 3
LINE REPLACEABLE UNITS ............................................................... 4
Transmitter ............................................................................................................4
Bracket ..................................................................................................................5
Remote Control Panel ...........................................................................................5
Outside antenna ....................................................................................................6
SYSTEM FUNCTIONAL DESCRIPTION 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 .................................................................108
Remote Control Panel RC200 Functional Description ...................... 109
General ..............................................................................................................109
RC200 Controls and Connector .........................................................................109
RC200 Working mode information .....................................................................110
Remote Control ...............................................................................................110
Monitoring .......................................................................................................110
RC200 Technical Characteristics ......................................................................110
Mechanical characteristics ..............................................................................110
Electrical Characteristics .................................................................................111

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Electrical Interfaces ......................................................................................... 111
RC200 Technical Specifications ........................................................................ 112
Photovoltaic Relay .......................................................................................... 112
Environmental specifications .......................................................................... 112
Antennas Technical Specifications .................................................................... 113
ANT 200 .......................................................................................................... 113
ANT 300 .......................................................................................................... 113
Equipment limitations ........................................................................ 113
Activation .......................................................................................... 114
Standby mode for automatic activation ............................................................. 114
Manual activation .............................................................................................. 114
Reset ................................................................................................. 114
Manual reset ...................................................................................................... 114
Reset with Remote Control Panel ..................................................................... 114
Self-Test ............................................................................................ 114
INSTALLATION / REMOVAL ............................................................. 201
Registration ....................................................................................... 201
General .............................................................................................................. 201
Registration 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 Installation .......................................................................... 208
Antenna Installation Recommendations ............................................................ 208
FAA Recommendations .................................................................................. 208
RTCA DO-204 Requirements ......................................................................... 208
Antenna mounting location ................................................................................ 208
Antenna installation procedure .......................................................................... 209
RCP installation ................................................................................ 210
RCP Installation Recommendations .................................................................. 210
RCP Installation Procedure ............................................................................... 210
Installation on the instrument panel ................................................................ 210
Installation below the instrument panel ........................................................... 211

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TABLE OF CONTENTS
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Connection ...................................................................................................... 212
ELT Connection ................................................................................ 213
First power up ................................................................................... 213
Removal ............................................................................................ 214
CHECK ............................................................................................... 301
Self-test ............................................................................................. 301
Periodicity .......................................................................................................... 301
Self-test procedure ............................................................................................ 301
Operational tests ............................................................................... 302
ELT operational tests ........................................................................................ 302
RCP operational tests ....................................................................................... 302
406 and 121.5 MHz transmission test ............................................................... 303
406 MHz ......................................................................................................... 303
121.5 MHz ...................................................................................................... 303
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
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 the control crash sensor ............................................................. 601
Transmitted signals ......................................................................................... 602
Batteries corrosion .......................................................................................... 602
Check of 121.5 MHz frequency ....................................................................... 602
6-year inspection ............................................................................................... 603
Visual control of the housing and accessories ................................................ 603
Operation of the controls and crash sensor .................................................... 603

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KANNAD 406 AF-COMPACT
TABLE OF CONTENTS
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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

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KANNAD 406 AF-COMPACT
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INTRODUCTION
The KANNAD 406 AF-COMPACT has been designed to satisfy the
requirements of general aviation pilots, built on the long experience of
KANNAD ELTs in 406 MHz technology in aviation, maritime and land distress
beacons.
The instructions in this manual provide the information necessary 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.
Foraquickviewofinstallation,pleaserefertoQuickInstallationGuidesupplied
with KANNAD 406 AF-COMPACT.
Antenna is not repairable and must be replaced if damaged.
FOR REGULATORY REQUIREMENTS, PLEASE CONSULT YOUR
NATIONAL AVIATION AUTHORITY.

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KANNAD 406 AF-COMPACT
PAGE INTRO 2
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WARRANTY
1. Scope
The equipment is warranted against all material or manufacturing defect for a
period of two years from the date of installation on the aircraft or thirty months
for the date of shipment from KANNAD S.A.S. Z.I. des Cinq Chemins BP23,
56520 Guidel, France, whichever occur first.
Work carried out under the warranty shall not have the effect of extending the
warranty period.
In respect of this warranty, after a defect has been noted by our services, the
sole obligation incumbent upon us shall be the repair 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. Exclusion
Defects and deterioration caused by natural wear of the product or by external
accident (poor maintenance, abnormal conditions of use, etc.) or by
modification of the equipment and tools not recommended nor specified by our
company, are excluded from the warranty.
Also the warranty shall not cover visible defects which the purchaser wouldn't
have formally notified KANNAD within 48 hours of receipt of the equipment.

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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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KANNAD 406 AF-COMPACT
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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 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;
• anti-deflagration;
• 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 achieved 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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KANNAD 406 AF-COMPACT
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2. KANNAD 406 ELTs Presentation
The KANNAD 406 AF-COMPACT belongs to the AF type of ELTs which are
permanently attached to an aircraft. The KANNAD 406 AF-COMPACT is
designed to be installed on fixed wing aircraft or helicopters.
The KANNAD 406 AF-COMPACT Pack is composed of:
1. 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.
Thetransmitter andbracketare installedintheaircraft nearthetail.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 3-wire bundle (not
supplied).
Figure 2: ELT system description

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KANNAD 406 AF-COMPACT
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3. LINE REPLACEABLE UNITS
A. Transmitter
The KANNAD 406 AF-COMPACT is an ELT designed to be installed onboard
aircraft to transmit a distress signal on frequencies:
• 406 MHz (COSPAS-SARSAT frequency) for precise pinpointing and
identification of the aircraft in distress.
• 121.5 MHz used for homing in the final stages of the rescue operations.
The 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 housing is designed with no sharp edges. It can be easily taken in one
hand.
Figure 3: KANNAD 406 AF-COMPACT Transmitter

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KANNAD 406 AF-COMPACT
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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.
Figure 4: KANNAD 406 AF-COMPACT with Mounting Bracket
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 9Pts connector
on the other side.
Note: the 3-wire cable is not supplied.
Figure 5: RC200 Remote Control Panel

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D. Outside antenna
The outside antenna can be either of whip (ANT200, P/N 0141013) or rod
(ANT300, P/N 0124220) 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 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 Antenna
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