04E66260C_USER`S HANDBOOK adt 406 S_rev-C

Transcription

USER’S HANDBOOK
INCLUDING INSTALLATION MANUAL
AND LOG BOOK
SERIAL NUMBER LABEL
EMERGENCY LOCATOR TRANSMITTER
MODEL ADT 406 S (P/N 01N65920)
IN THE COSPAS / SARSAT SYSTEM
Issued by
ELTA
F6614
14 Place Marcel Dassault
31702 BLAGNAC
France
www.elta.fr
Documentation P/N: 04E66260 Rev C
Initial issue: June 6/05
Title Page
May 20/10
LIST OF UPDATES
UPDATE
No.
INSERTION
ISSUE
DATE
June 6/05
BY
E.LABRIFFE
A
INITIAL
B
Update,
Apr. 25/08 C. CRESP
Canadian
Approval &
new mounting
bracket
C
Update
ELT Removal
Installation &
new Canada
Coding Label
UPDATE
No.
INSERTION
ISSUE
DATE
BY
May 20/10 C.CRESP
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TABLE OF ILLUSTRATIONS
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LEADING PARTICULARS
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TABLE OF ILLUSTRATIONS
Page
Figure 1 : COSPAS/SARSAT - System Principle
12
Figure 2 : ELT ADT 406 S (P/N 01N65920) - Presentation
Secured on standard mounting bracket (P/N 04N64250)
15
Figure 3 : ELT ADT 406 S (P/N 01N65920) - Overall Dimensions
On standard mounting bracket (P/N 04N64250)
16
Figure 4 : ELT ADT 406 S (P/N 01N65920) - Presentation
Secured on alternative mounting bracket (P/N 07N62351
17
Figure 5 : ELT ADT 406 S (P/N 01N65920) - Overall Dimensions
Secured on alternative mounting bracket (P/N 07N62351)
18
Figure 6 : ELT ADT 406 S – Overall Dimensions (Storage & transportation bag)
19
Figure 7 : Installation of the ELT ADT 406 S mounting brackets - Drilling Patterns Dimensions
28
Figure 8 : ELT ADT 406 S (P/N 01N65920) on standard mounting bracket (P/N 04N64250)
Detailed Description
52
Figure 9 : ELT ADT 406 S (P/N 01N65920) on standard mounting bracket (P/N 07N62351)
Detailed Description
53
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LEADING PARTICULARS
CAUTION 1 : THIS TRANSMITTER IS AUTHORIZED FOR USE ONLY DURING SITUATIONS OF GRAVE
AND IMMINENT DANGER.
CAUTION 2 : IT IS IMPERATIVE THAT EACH ADT 406 S TRANSMITTER OWNER REGISTERS THEIR
ADT 406 S TRANSMITTER. CONTACT YOUR LOCAL AIRWORTHINESS AUTHORITY TO
OBTAIN THE INFORMATION RELATIVE TO THIS REGISTRATION. ELTA OR APPROVED
AGENT MAY HELP YOU IN THAT PROCESS.
CAUTION 3 : THE ADT 406 S TRANSMITTER MUST BE MPERATIVELY PROGRAMMED WITH THE
UNIQUE & RELEVANT IDENTIFICATION AUTHORIZED BY THE LOCAL
AIRWORTHINESS.
CAUTION 4 : ONCE THE ADT 406 S TRANSMITTER HAS BEEN PROGRAMMED, IT IS GENERALLY
ASSIGNED TO AN AIRCRAFT (NAME AND IDENTIFICATION). IF THIS ADT 406 S
TRANSMITTER IS USED ON ANOTHER AIRCRAFT, IT HAS TO BE REPROGRAMMED
(NEW NAME AND IDENTIFICATION).
CAUTION 5 : BEFORE INSTALLING OR USING THIS EQUIPMENT, THE VALIDITY OF THE
INFORMATION ON THE ADT 406 S TRANSMITTER LABEL MUST BE IMPERATIVELY
CHECKED.
CAUTION 6 : WHEN THE ELT IS MOVED TO AN OTHER A/C, IDENTIFICATION MUST BE CHECKED IN
ORDER TO MEET LOCAL AIRWORTHINESS REQUIREMENT
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TABLE OF CONTENTS
PAGE
1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM
A. The COSPAS-SARSAT system
B. System organization
C. The distress frequencies
D. ELTA and the COSPAS-SARSAT system
2. GENERAL CHARACTERISTICS OF THE ELT ADT 406 S
A. Purpose of the ELT ADT 406 S
B. Characteristics
3. DESCRIPTION OF THE ELT ADT 406 S
A. General description
B. Detailed description
4. INSTALLATION OF THE ELT ADT 406 S
A. General
B. Installation of the ADT 406 S transmitter on the aircraft
C. Installation and configuration of the ADT 406 S transmitter
5. UTILIZATION OF THE ELT ADT 406 S
A. Water activation
B. Manual activation
C. ELT ADT 406 S Operation and Manipulation Clarification
D. ELT ADT 406 S Removal/Installation from mounting bracket P/N 04N64250
E. ELT ADT 406 S Removal/Installation from mounting bracket P/N 07N62351
F. ELT ADT 406 S Removal/Installation from storage and transportation bag P/N 04N64255
G. ADT 406 S transmitter shutdown
H. ADT 406 S transmitter self-test
6. MAINTENANCE OF THE ELT ADT 406 S
A. ADT 406 S transmitter self-test
B. Water Sensor test
C. Maintenance periodicity table
D. Battery replacement
E. Battery discarding
F. Test to be performed at the time of a ADT 406 S transmitter return in workshop
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1. INTRODUCTION TO THE COSPAS-SARSAT SYSTEM
A. The COSPAS-SARSAT* system
The purpose of the COSPAS-SARSAT satellite system is to detect and locate all distress signals
transmitted by aeronautical, maritime or land-based ADT 406 S transmitters, for the search and rescue
organizations.
Developed through the international collaboration of the United States, Canada and France the SARSAT
2
1
project is fully compatible with the Russian based COSPAS project .
Since the first results were obtained several countries have joined the program. Several other countries
have shown an interest and will soon be joining the COSPAS-SARSAT system partners.
ELTA in relation with CNES (French National Space Agency) has developed the complete range of
products required for COSPAS-SARSAT system operation.
Following an in-depth study phase, ELTA has achieved at highly conclusive technical results.
Experimental and operational use of the "ground" equipment have proven this equipment's reliability and
ease-of-use.
B. System organization (Ref. Fig. 1)
In the COSPAS-SARSAT system, space equipment is placed on board several satellites in low nearpolar orbit to capture transmissions from emergency transmitters and to retransmit these signals to
specialized ground stations called Local User Terminals (LUT). These ground stations determine the
position of the emergency transmitters and then retransmit the position data to the designated Mission
Control Centers (MCC). The MCCs in turn retransmit these data to the appropriate Rescue Coordination
Centers (RCC) so that they can start the search and rescue operations.
*
COSPAS-SARSAT :
1
COSPAS = Kosmicheskaya Sistyema Poiska Avariynych Sudov
2
SARSAT = Search and Rescue Satellite-Aided Tracking
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Legend :
ELT : Emergency Locator Transmitter
EPIRB : Emergency Position Indicating Radio ADT 406 S transmitter
PLB : Personal Locator ADT 406 S transmitter
RCC: Rescue Coordination Centers
MCC: Mission Control Centers
LUT : Local User Terminals
COSPAS/SARSAT – System Principle
Figure 1
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C. The distress frequencies
There are several advantages using the 406 MHz frequency :
– Worldwide coverage: detecting location is not only possible in real-time within a radius of about 2,500
km [1350 nmi] around the station, but also in global mode outside this zone since the satellites
memorize the messages on the 406 MHz frequency. Location process uses Doppler effect.
– Locating accuracy: less than 2 km [1 nmi] as opposed to 10 [5.4 nmi] to 15 km [8 nmi] in the 121.5
MHz or 243 MHz frequencies. It should be noted however, that the 406 MHz ADT 406 S transmitters
also transmit 121.5 MHz and 243 MHz signals, which enable the final approach of the rescue teams in
homing mode.
– Information reliability: the structure of the digital signal transmitted by these ADT 406 S transmitters
makes it possible to verify that there is a distress situation, as well as to automatically identify the
means of transport in distress, which is vital for search and rescue operations.
– Unique identification: each ADT 406 S transmitter has its own identification information.
D. ELTA and the COSPAS-SARSAT system
(1) 406 MHz distress ADT 406 S transmitter:
These ADT 406 S transmitters transmit to the satellites a digital message which identifies them and
gives their position, as well as a signal that facilitates the final approach of the rescue teams.
They are suitable for all types of use (maritime, aeronautical and land) and can, depending on the
model, be activated manually or automatically. They are designed to function in the most extreme
conditions with a high degree of reliability.
(2) Satellites low earth orbiting:
At least four satellites are permanently operational with their orbit at near-polar. In the worst case every
point on Earth is overflown every two hours.
In a ground station's visibility zone, the satellites directly transmit the messages captured in that zone,
in addition to any other messages stored in memory found within the zones that are not covered.
Geo-stationary satellites : now available in the system and offer faster detection capability (close to 4
minutes of angle), but require a GPS receiver to supply actual location that is sent via C/S message.
(3) Ground reception stations:
The zone effectively covered (visibility zone) is a circle with a radius of about 2,500 km [1350 nmi]
around the station. These stations receive via the satellite and process the messages in real time from
the ADT 406 S transmitters activated in their visibility zone and the memorized messages.
Automatic processing of the 406 MHz digital messages allows the ADT 406 S transmitters to be
located and the carrier mobile to be identified.
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USER’S HANDBOOK
2. GENERAL CHARACTERISTICS OF THE ELT ADT 406 S
A. Purpose of the ELT ADT 406 S (Ref. Fig. 2)
The ELT ADT 406 S consists of a ADT 406 S transmitter secured on an optional mounting bracket that
incorporates means of attachment or inside an optional storage and transportation bag.
The ELT ADT 406 S is designed to transmit a digital distress signal to satellites that are part of the
COSPAS/SARSAT SYSTEM.
These satellites transmit the captured signal to the reception stations on the ground.
This signal is transmitted on the 406.028 MHz frequency and is used to precisely locate and identify the
ELT ADT 406 S.
It also transmits a 121.5 MHz and 243 MHz homing signal to facilitate the final approach of the distress
scene (homing process).
It can be manually or automatically triggered by means of a water sensor (fresh or salted).
This ELT meets the latest JAR/E OPS and ICAO recommendations.
Any encoding protocol defined by COSPAS/SARSAT can be used with ELT ADT 406 S, including country
code assignment.
The purpose of the Activation/Identification module on the top of the ELT transmitter is to store on board
the A/C the Cospas-Sarsat identification. This module is attached to the A/C structure by the metallic
strap. It will keep on board the A/C the Cospas-Sarsat code. This module is transferable i.e. can be
installed after removal on a new ELT transmitter (from the shop for maintenance as example). The
operator is sure that the new ELT transmitter will transmit the correct Cospas-Sarsat message upon
activation.
The identification code is stored in the non volatile memory and will not be lost upon module or battery
removal. The automatic activation is based on a water sensor.
The ADT 406 S ELT is a non-location protocol ELT and does not have the capability to determine or
transmit its own location.
If the ownership change, the ELT shall be re-coded (new 15 digit Hex Code) with the appropriate country
code and coding protocol as selected or required by the country of the new final operator. Contact ELTA
for additional details (www.elta.fr ).
Note for CANADIAN owners:
The selected Cospas-Sarsat protocol must be the “Aircraft 24 bit address”.
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Activation
Identification
Module (AIM)
(Water sensor)
Metallic strap
Note 1 :
Metallic strap is
used to retain
AIM on A/C
(normal
operation)
ELT ADT 406 S (P/N 01N65920) - Presentation
Secured on standard mounting bracket (P/N 04N64250)
Figure 2
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Optional
Protective Cover
(P/N 04N64265)
(Transparent LEXAN)
ELT ADT 406 S (P/N 01N65920) - Overall Dimensions
On standard mounting bracket (P/N 04N64250)
(Protective cover is optional)
Figure 3
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An alternative solution exist when the available space around the ELT is limited. With this solution the
ELT transmitter can be removed from the front.
Activation
Identification
Module (AIM)
(Water sensor)
Metalic strap
Note 2 :
Metallic strap is
used to retain
AIM on A/C
(normal
operation)
ELT ADT 406 S (P/N 01N65920) - Presentation
Figure 4
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ELT ADT 406 S (P/N 01N65920) - Overall Dimensions
Figure 5
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Optional Storage and Transportation bag:
ELT ADT 406 S Storage & Transportation Bag (P/N 04N64255)
Overall Dimensions
Figure 6
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B. Characteristics (Ref. Fig. 3)
(1) Approvals
ADT 406 S is COSPAS/SARSAT approved (TAC 153, dated 15 sep. 2005, updated 2007)
ADT 406 S meets EUROCAE ED62, RTCA DO-204, RTCA DO-183 standards
ADT 406 S is ETSO 2C91a and ETSO 2C126 approved (ETSO N° EASA.21O.353 dated October 12,
2005, updated 14 September 2007 [minor modification])
ADT 406 S is TSO C91a and TSO C126 approved (TSO letter dated January 9, 2006 )
(2) Physical characteristics
(a) ADT 406 S transmitter (P/N 01N65920) on standard mounting bracket (P/N 04N64250)
Height : 105 mm [4.14 in]
Width : 185 mm [7.28]
Length : 295 mm [11.61 in] (with optional plastic cover P/N 04N64250)
Weight : - ADT 406 S transmitter (with antenna) : 1.6 Kg [3.52 lbs]
- Standard mounting bracket : 0.34 kg [0.75 lbs]
- Optional protection cover : 0.04 Kg [0.08 lbs]
(b) ADT 406 S transmitter (P/N 01N65920) on alternative mounting bracket (P/N 07N62351)
Width : 191 mm [7.53]
Length : 266 mm [10.47 in]
Weight : 1.6 Kg [3.52 lbs], ADT 406 S transmitter (with antenna)
-
Alternative mounting bracket : 0.45 kg [0.994 lbs]
-
Optional protective cover (P/N 04N64250) not compatible with this alternative
mounting bracket
(c) ADT 406 S transmitter only
Width : 185 mm [7.28 in]
Length : 221.5 mm [8.72](without antenna)
Weight : 1.6 Kg [3.52 lbs] ADT 406 S transmitter (with antenna)
Length with antenna deployed : 540 mm [21.26 in]
(d) Optional storage and transportation bag
Width : 205 mm [8.07 in]
Length : 300 mm [11.81]
Weight : 0.3 Kg [0.74 lbs]
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(3) General characteristics
(a) Whip antenna
– Omni-directional three-frequency antenna TNC 50Ω access
– In compliance with COSPAS/SARSAT and EUROCAE ED-62 specifications
(b) Power supply
High energy batteries (2 series-connected packs), activable for 5 years. Autonomy 24 hours on
406.028 MHz and greater than 48 hours at -20°C on 121.5&243 MHz.
–
–
–
–
–
Voltage
: 6 VDC,
capacity
: 10.5 A/h,
ELTA type number
: 00E64191,
lithium manganese dioxide LiMNO2 (solid cathode),
battery servicing kit available: 05N62123 kit for one ELT.
(c) Radio-electrical characteristics
1 406 MHz satellite transmitter
–
–
–
–
–
Frequency
: 406.028 MHz
transmitter power
:5W
modulation
: "L" two-phase
transmission recurrence : 50 s
transmission duration : 440 ms
2 Associated homing transmitter
–
–
–
–
Frequency
121.5 MHz transmitter power
243 MHz transmitter power
modulation
– antenna gain
: 121.5 MHz/243 Mhz
: typical 100 mW
: typical 100 mW
: AM (3K20A3X type) from, 1600 Hz to 300 Hz
up to four periods per second
: 1 dBi
(d) Environment characteristics
– Operating temperatures : -20°C to +55°C
– Storage temperatures
: -55°C to +85°C
– Ambient temperature (20°C) is highly recommended for storage in order to reduce self discharge
of the batteries, when the equipment is equipped with internal batteries
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(e) Miscellaneous characteristics
– Automatic activation by water sensor in armed mode (fresh or salted)
The water sensor is located on the “Activation/Identification” module. It is constituted by two
metallic plugs that must be immerged to allow the automatic activation when the ELT is in a float
free condition. Water activation is memorized and the ELT will continue to transmit once
activated even if removed from water. Water sensor is designed to operate either in fresh or
salted water condition. For a correct activation the water sensor must be totally immerged for
more than 2 seconds avoiding false activation in case of “ELT splash”. The
“Activation/Identification” module is made of of plastic (PEEK 1000) that will not keep water on it
unless it is immerged.
– color
:
orange in conformity with the international distress signal
– self-test
:
Separate self test push button, only active in “ARMED” position
Transmission of one 406.028 MHz burst modulated with inverted
frame synchronization,
and 5s transmission of 121.5 MHz .
– any COSPAS/SARSAT protocol available,
. ELT S/N
. A/C operator designator and S/N
. A/C 24 bits address
. A/C nationality and registration marking (recommended)
. Test
– any country code available
– operate in short C/S message only
– C/S identification stored in a transferable module to ease maintenance on ELT (Activation /
Identification Module)
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3. DESCRIPTION OF THE ELT ADT 406 S
A. General description
(1) Introduction
This ADT 406 S transmitter is based from the ADT 406 AF/AP model. Consequently, this ADT 406 S
transmitter features the functional capabilities of the AF/AP. In addition to its flotation part, the
attachment interface and its flexible antenna are entirely compatible with Cospat/Sarsat for a Survival
application.
(2) The ELT ADT 406 essentially consists of :
–
–
–
–
–
–
ADT 406 S transmitter
whip antenna
labels
Activation / Identification Module
mounting brackets or storage/transportation bag
optional protection cover (for standard mounting bracket only)
B. Detailed description (Ref. Fig. 8 or Fig 9)
(1) The ADT 406 S transmitter
The ADT 406 S transmitter mainly consists of :
–
–
–
–
–
whip antenna
power supply module
electronic assembly
mechanical assembly
float element
The front face of the electronic assy is equipped with the following components :
–
–
–
–
WHIP ANT. TNC female connector (1) for connecting up the antenna
ARMED/OFF/ON lockable toggle switch (3) for activating the ADT 406 S transmitter
TEST push button (12) for ADT 406 S transmitter self test
TX indicator light (2) indicating ADT 406 S transmitter activation (real distress and self-test
process)
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(2) The labels
(a) Identification label
The labels indicate:
– ADT 406 S transmitter name, manufacturer details
– operational condition in which the ADT 406 S transmitter is intended to be used (warning)
– approval number, identification, part number, service bulletin, serial number and RTCA DO160 qualification level of the ADT 406 S transmitter
FCCID:LYJADT406S
Serial number label
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(b) ADT 406 S transmitter front panel label
This label indicates the switches operations and the location of the connector on the front face of the
electronic assembly.
(c) Identification label
This label is fixed onto the Activation / Identification Module.
Simplified
C/S identification
XXX...XX
XXX...XX
XXX...XX
Official 15 Hex.
C/S identification
Aircraft assignation
(d) Batteries label
This label indicates the batteries’ expiration date (next battery servicing).
(e) Dedicated “Canadian Application” labels
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Two additional labels are stuck on the ELT for this application.
One is related to “Cospas-Sarsat” matters in CANADA
One is related to “Battery part clarification” for CANADA
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4. INSTALLATION OF THE ELT ADT 406 S
A. General
System safety and reliability obviously depend on the standard of installation.
In order to ensure installation to the highest standard, the installation operations must be:
–
–
–
–
performed in conformity with this document
performed in compliance with the current regulations
performed by qualified personnel
performed so that :
. the aircraft's structural integrity is not affected
. it will not hinder the pilot in normal position
. it will not cause any damage in the event of an accident
. it will not prevent or modify operation of the other safety systems
If in doubt, contact the aircraft manufacturer or its representative
– inspected by representative authority
B. Installation of the ADT 406 S transmitter on the aircraft (Ref. Fig. 7)
The ADT 406 S transmitter can be installed in any position in the aircraft, but the switch and the
Activation / Identification module must be protected from passengers to exclude false activations.
Unstowed objects must be not able to impact the ADT 406 S transmitter.
When installed on a mounting bracket, the ADT 406 S transmitter must be attached to the fuselage of
the aircraft by means of four M4 bolts. Four 5 mm diameter holes at the corners of a 210 mm x 45 mm
rectangle are drilled into the ADT 406 S transmitter mounting bracket. Particular care must be taken with
this attachment. Standard industry means must be used to lock the screws. Use flat washer in order to
avoid paint damage on the mounting bracket.
The attachment points are identical to those of the ADT 406 AF/AP ADT 406 S transmitter (same drilling
pattern).
When the operator uses the storage and transportation bag, the metallic strap from the
Activation/Identification Module can not be secured to the A/C.
In that case we recommend that the operator create and stuck a label on the storage & transportation
bag indicating that this type of ELT is normally encoded and assigned to a dedicated A/C unless the
Cospas-Sarsat protocol selected is “ELT serial number” In that case of ELT serial number protocol
selection the ELT identification is not related to the A/C but the operator must inform its local
Airworthiness Authority of any ELT move (new registration process).
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Figure 7 shows the drilling pattern dimensions and determines the required area to access to the ADT
406 S transmitter controls and connectors.
ELTA recommended mounting bracket configuration
Use of other drilling pattern is possible for existing ADT 406 S transmitter Retrofit only
(contact ELTA for detailed information)
Installation of the ELT ADT 406 S mounting brackets - Drilling Patterns Dimensions
Figure 7
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C. Installation and configuration of the ADT 406 S transmitter (Ref. Fig. 8 or 9)
(1) Installation in automatic survival mode (water activation)
CAUTION : TO BE OPERATIONAL, THE ADT 406 S TRANSMITTER SHALL BE IN "ARMED"
POSITION ONCE IT HAS BEEN CORRECTLY INSTALLED.
Make sure that the antenna is correctly connected to the TNC connector.
Move the ADT 406 S transmitter ARMED/OFF/ON lockable toggle switch to the “ARMED” position (pull
and slide) so that the system is ready for use. The water sensor is then operational and will activate the
transmitter when it is floating on water (fresh or salted).
CAUTION : AS SOON AS THE ADT 406 S TRANSMITTER IS IN ARMED, IT CAN BE
AUTOMATICALLY ACTIVATED BY THE WATER SENSOR .
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5. UTILIZATION OF THE ELT ADT 406 S (Ref. Fig. 8 & Fig. 9)
CAUTION : IN THE EVENT OF AN UNTIMELY ADT 406 S TRANSMITTER ACTIVATION, SHUTDOWN
THE ADT 406 S TRANSMITTER AND INFORM THE CLOSEST SEARCH AND RESCUE
(SAR) OR AIRPORT CONTROL TOWER IMMEDIATELY.
The ELT ADT 406 S can be activated in two modes :
– automatic when the water sensor is triggered
– manual
A. Water activation
The aircraft has to be evacuated, the ADT 406 S transmitter is removed from its mounting bracket or
storage/transportation bag and dipped into the water by the cabin crew member or passenger.
The water sensor has detected sufficient water to trigger it. The indicator light (2) and the aural indicator
indicate ADT 406 S transmitter activation.
It is recommended to secure the ADT 406 S transmitter to a survivor or life raft using the lanyard.
Do not do anything and leave the ADT 406 S transmitter in operation until the rescue team arrives.
B. Manual activation
There are two cases in which a distress signal may be triggered manually:
– the water sensor has not been triggered, but a distress signal must be sent (injured passengers,
aircraft out of operation)
– the aircraft is on the ground and must be evacuated
From the ADT 406 S transmitter front panel :
Move the ADT 406 S transmitter switch (3) to the “ON” position (pull and slide), and do not do anything
else.
An automatic self-test sequence is performed completed with the self test report display on indicator
light (2).
Then the ADT 406 S transmitter is positioned in a waiting condition for about 30s. This state is
displayed by flashings on indicator light (2) 1.75 s ON, 0.25 s OFF. This delay will avoid unwanted
activation (false maneuver).
Then the indicator light (2) and the aural indicator indicate the ADT 406 S transmitter activation. The
actual distress signal are transmitted. This state is displayed by flashing on indicator light : 0.5 s
ON, 0.5 s OFF.
CAUTION : IN THE TWO CASES OF ACTIVATION, MAKE SURE THAT THE ANTENNA IS FULLY
DEPLOYED AND IN VERTICAL POSITION. FOR MAXIMUM POWER TRANSMISSION THE
ANTENNA MUST BE IN AN UNOBSTRUCTED AREA FAR FROM ANY METALLIC PIECES.
Page 30
May 20/10
USER’S HANDBOOK
C. ELT ADT 406 S Operation and Manipulation Clarification
For a crash at sea the ADT 406 S transmitter will activate automatically when dipped into water should
the ELT front panel toggle switch ON OFF ARMED is placed in ARMED position.
For a crash on ground the ADT 406 S transmitter will be activate manually when the ELT front panel
toggle switch ON OFF ARMED is placed in ON position.
It is recommended to place the ADT 406 S transmitter in an unobstructed area (avoiding transmission
masks), and check regularly that the antenna remains vertical. If necessary secure the ADT 406 S
transmitter vertically (e.g. in case of windswept area).
The ELT is designed to transmit in any configuration:
•
Floating on water (Float Free Configuration),
•
Standing on ground (Terrestrial configuration),
•
Held by Survivor hand.
The best data transmission of the ADT 406 S transmitter is obtained in water floating conditions (do not
forget to anchor the ADT 406 S transmitter to the survivors or to the life raft with the orange lanyard
attached to the ADT 406 S transmitter front panel).
Warning: When the whip antenna is deployed it should not be used to carry the ELT as indicated here under.
Whip antenna damage will occur.
NOT OK
Page 31
May 20/10
USER’S HANDBOOK
The ELT should be held by one of the protective metallic arch or by the ELT case
(See here under correct example)
OK
D. ELT ADT 406 S Removal/Installation from mounting bracket P/N 04N64250
(1) ELT Removal instructions:
ELT Transmitter installed on the Mounting Bracket Assembly with its protective cover (starting point)
Page 32
May 20/10
USER’S HANDBOOK
Step1. Remove the protective cover and Grasp the Velcro strap away from the ELT case. This action
should also disconnect the metallic snap fastener.
Step 2. Rotate the ELT case and slide it to the left in order to disengage the protective metal arch from
the locker position made on the mounting bracket.
Page 33
May 20/10
USER’S HANDBOOK
Step 3. Grasp the ELT case or one of the protective metal arches and pull the ELT Transmitter directly
away from mounting bracket, automatically deploying the spring loaded flexible whip antenna.
Take care not to place body parts in proximity to the antenna during deployment or injury may result.
Warning: Do not use the whip antenna as a “handle” to manipulate the ELT
NOTE : Do not elevate the ELTA case before the removal of the flexible whip antenna from the mounting
bracket foam in order to ovoid blockage resulting in acute angle that may damage the flexible whip antenna.
Page 34
May 20/10
USER’S HANDBOOK
The ELT Transmitter has been removed from mounting bracket and whip antenna automatically deployed. ELT
transmitter is ready for distress signalling (See chapter C “ELT ADT 406 S Operation and Manipulation
Clarification” above) or maintenance activities.
Page 35
May 20/10
USER’S HANDBOOK
(2)ELT Installation instructions:
The ELT Transmitter is shown with flexible whip antenna deployed (Starting point)
ELT is held using one of the protective metallic arches or ELT Transmitter housing itself
Step 1 Carefully bend the flexible whip antenna under the ELT transmitter and direct the whip antenna
into the provided slot in the foam until it bottoms against the bottom of the foam.
Page 36
May 20/10
USER’S HANDBOOK
Step 2 Rotate the ELT case and engage the protective metal arch from the locker position made on
the mounting bracket
Step 3 Seat ELT Transmitter into bracket with bottom of transmitter housing against the bottom of the
bracket. Place the Velcro strap in the metallic loop and compress the assembly.
Page 37
May 20/10
USER’S HANDBOOK
Step 4 Attach hooks and loops of the velcro strap on the top of the ELT case and secure the fastener
snap.
The ELT Transmitter as shown below has been correctly installed on the Mounting Bracket Assembly without
stressing or compressing the flexible whip antenna.
Step 4 Install the protective cover. It will secure and protect the radius of the flexible whip antenna to its
standard fit.
NOTE: The proper bend radius for the whip antenna is approximately 6 cm (2.32 inches)
Page 38
May 20/10
USER’S HANDBOOK
E. ELT ADT 406 S Removal/Installation from mounting bracket P/N 07N62351
ELT Transmitter installed on the Mounting Bracket Assembly (starting point)
Step1. Grasp and “PULL” the Velcro strap handle away from the ELT control panel as shown. This action
should also disconnect the two metallic snap fasteners.
Page 39
May 20/10
USER’S HANDBOOK
Step 2. Grasp one of the protective metal arches and pull the ELT Transmitter directly away from
mounting bracket, automatically deploying the spring loaded flexible whip antenna. Take care not to place body
parts in proximity to the antenna during deployment or injury may result.
The ELT Transmitter has been removed from mounting bracket and whip antenna automatically deployed. ELT
transmitter is ready for distress signalling (See chapter C “ELT ADT 406 S Operation and Manipulation
Clarification” above) or maintenance activities.
Page 40
May 20/10
USER’S HANDBOOK
Step 1(a) Carefully bend the flexible whip antenna under the ELT transmitter and direct the whip
antenna into the provided slot in the foam until it bottoms against the bottom of the bracket.
Page 41
May 20/10
USER’S HANDBOOK
Step 1(b) Seat ELT Transmitter into bracket with bottom of transmitter housing against the bottom of
the bracket.
Step 2 Place the two Velcro straps across the top of the transmitter as shown
Page 42
May 20/10
USER’S HANDBOOK
Step 3 Compress the ELT foam with the first rear Velcro strap (Use yellow tab with one hand).
Attach the corresponding front Velcro strap and secure it with the metallic snap fastener.
Step 4 Compress the ELT foam with the second rear Velcro strap (Use yellow tab with one hand)
Page 43
May 20/10
USER’S HANDBOOK
Step 5 Attach the remaining front Velcro strap and secure it with the metallic snap fastener.
The ELT Transmitter as shown below has been correctly installed on the Mounting Bracket Assembly without
stressing or compressing the flexible whip antenna..
NOTE: The proper bend radius for the whip antenna is approximately 6 cm (2.32 inches)
Page 44
May 20/10
USER’S HANDBOOK
F. ELT ADT 406 S Removal/Installation from storage and transportation bag P/N 04N64255
Survivors must exit from the A/C with the storage and transportation bag
When you are in a safe location:
Step 1. Open the storage and transportation bag and Remove the upper foam protective part
Step 2. Grasp one of the protective metal arches and pull the ELT Transmitter directly away from the
storage & transportation bag, automatically deploying the spring loaded flexible whip antenna.
Take care not to place body parts in proximity to the antenna during deployment or injury may result.
The ELT Transmitter has been removed from Storage and Transportation bag and whip antenna automatically
deployed. ELT transmitter is ready for distress signalling (See chapter C “ELT ADT 406 S Operation and
Manipulation Clarification” above) or maintenance activities.
Page 45
May 20/10
USER’S HANDBOOK
Step 1 Carefully bend the flexible whip antenna behind the ELT transmitter and direct the whip
antenna into the provided slot in the back of the storage and transportation bag.
Then slide down the ELT inside the storage and transportation bag and verify that it correctly seats in
the bottom foam part as indicated in the last picture here under.
Page 46
May 20/10
USER’S HANDBOOK
Step 2 Install the upper protective foam and verify its correct location. Then close the Storage and
Transportation Bag.
G. ADT 406 S transmitter shutdown
In the event of a false maneuver or untimely operation, shutdown the ADT 406 S transmitter.
The ADT 406 S transmitter is shutdown by placing the ARMED/OFF/ON toggle switch (3) in OFF
position.
CAUTION : THE ADT 406 S TRANSMITTER MUST BE SHUTDOWN BEFORE ANY MAINTENANCE
OPERATIONS ARE PERFORMED.
THE ADT 406 S TRANSMITTER MUST BE COMPLETELY SHUTDOWN BEFORE IT IS
REMOVED FROM THE AIRCRAFT, ESTABLISHING THAT ITS ARMED/OFF/ON
TOGGLE SWITCH IS IN OFF POSITION.
H. ADT 406 S transmitter self-test
CAUTION : THE SELF-TEST SHALL BE PERFORMED WITHIN THE FIRST 5.MIN OF ANY HOUR
BECAUSE THE ELT IS SENDING A 121.5 MHZ SIGNAL FOR 5 S DURING THIS PROCESS
(LIMITATION OF FALSE ALERT).
The ELT ADT 406 S is designed to perform a self-test by using the TEST push button, when the
ON/OFF/ARMED toggle switch is in ARMED position.
Actual test transmission on 121.5 MHz for 5 s can be listened on any VHF receiver tuned on 121.5 MHz.
Even if the self test of the ADT 406 S transmitter is possible when it is installed on its mounting bracket,
we recommend to remove it from its mounting bracket or from the storage & transportation bag and to
deploy the antenna before performing the self test. Hold the ADT 406 S transmitter at arm’s length in the
aisle to free the antenna from metallic part.
Place the ADT 406 S transmitter's ARMED/OFF/ON toggle switch (3) in the “ARMED” position to
authorize the self test process.
Press TEST pushbutton (12) until the two acknowledgments blink on indicator light (2).
Page 47
May 20/10
USER’S HANDBOOK
After the two short blinks (acknowledgment) and a delay of 3 s, check that the indicator light (2) comes
ON and the ADT 406 S transmitter's buzzer sounds during 6s.
After a brief blink the self-test report is displayed on the indicator light (2):
– 10 s permanent illumination for correct operation
– 10 s blinking condition for failure detection
An easy way to detect the correct failure condition is simply to count the number of blinks during the 10
s self test report duration.
Blinking rate indicates the failure source detection as follow :
. 10 blinks i.e. 500 ms ON, 500 ms OFF (Frequency 1 Hz), Ext. Antenna connection failure or
identification missing (AIM can not be read),
. 20 blinks i.e. 250 ms ON, 250 ms OFF (Frequency 2 Hz), ELT power failure (UHF and/or VHF),
. 40 blinks i.e. 125 ms ON, 125 ms OFF (Frequency 4 Hz), ELT Check Sum failure (software
problem
Self test
Acknowledgement
6s Self Test process
10 s Self Test report
ADT 406 S transmitter self test diagram
The self test is finished and the ADT 406 S transmitter return in ARMED mode.
Fold up the antenna, return the ADT 406 S transmitter to its bracket and grip the strap
6. MAINTENANCE OF THE ELT ADT 406 S
A. ADT 406 S transmitter self-test
The manufacturer recommends that a ADT 406 S transmitter self-test should be performed regularly.
The highest rate is once per week. Generally, airlines add this task to other periodic maintenance tasks
such an “A” check. In all events the user must comply with the applicable regulations in the country
concerned governing the self-test period.
The self-test must only be performed when upon authorization or by the competent authorities.
A higher rate of self-testing will reduce the 5 years of battery servicing.
CAUTION :THE SELF-TEST PROCEDURE (PARAGRAPH 5.E.) MUST BE RESPECTED TO AVOID
UNTIMELY ADT 406 S TRANSMITTER ACTIVATION.
Page 48
May 20/10
USER’S HANDBOOK
B. Water Sensor test
The water sensor, located in the Activation/Identification Module, should be tested at the periodic
maintenance task. Place the ARMED/OFF/ON toggle switch (3) in the “ARMED” position, and make a
conductive connection between the two hexagonal socket screws of the water sensor assy.
This conductive connection must last 2 to 3 seconds to activate the ADT 406 S transmitter.
CAUTION: WHEN THE ADT 406 S TRANSMITTER IS ACTIVATED SWITCH OFF THE ADT 406 S
TRANSMITTER WITHIN 30S IN ORDER TO AVOID FALSE ALERT AND RETURN IT IN
ARMED IF NECESSARY. THE WATER SENSOR WORK CORRECTLY.
C. Maintenance periodicity table
Periodicity
Operations
Operator
5 years
Replacement of batteries
ELTA or approved agent/airline
5 years
General overhaul * in specialized
workshop
ELTA or approved agent/airline
* There is no real overhaul with the ELT as there is no parts that need replacement due to the ELT
normal operation (unless the battery packs). Of course damaged part such as antenna, float, labels …
can be replaced as necessary.
CAUTION: THE TWO BATTERY PACKS MUST BE REPLACED: AFTER USE OF THE ELT IN AN
EMERGENCY CONDITION OR AFTER AN INADVERTENT ACTIVATION OF UNKNOWN
DURATION OR BEFORE THE PROPOSED BATTERY REPLACEMENT DATE
INDICATED ON THE LABEL STUCK ON THE BOTTOM OF THE ELT
CAUTION: FOR MAINTENANCE PURPOSE, DURING SHIPPING OR TRANSPORT OF THE ELT
MAKE SURE THAT ELT TRANSMITTER FRONT PANEL TOGGLE SWITCH IS DULLY
SET IN ITS “OFF” POSITION AS INDICATED ON THE FRONT PANEL LABEL. THIS
VERIFICATION WILL AVOID FALSE ACTIVATION DURING TRANSPORT AND
MANIPULATION IF THE ELT REMAINS IN “ARMED”.
Page 49
May 20/10
USER’S HANDBOOK
D. Batteries replacement
CAUTION : THE BATTERY PACK SHALL BE APPROVED BY ELTA. IF OTHER PACKS ARE USED
ELTA WILL CANCEL WARRANTY AND WILL REFUSE ANY RESPONSIBILITY ON THE
PRODUCT OPERATION / MISFUNCTION.
CAUTION : THE BATTERIES USED CANNOT BE RECHARGED. DO NOT TRY TO OPEN OR
RECHARGE THEM.
CAUTION : BOTH OLD BATTERY PACKS MUST BE REPLACED WITH NEW FRESH ONE OF A
MODEL APPROVED BY ELTA.
Next battery servicing date is indicated on the label placed on the back face of ADT 406 S (month &
year).
Manufacturing date of the two new fresh battery packs must be the compatible (same manufacturing
batch).
P/N 05N62123 is the mandatory battery servicing kit for one ELT ADT406 S. It contents two fresh battery
packs and all the necessary consumable required for that operation.
ELTA recommends that the ELT ADT 406 S should undergo a general inspection (as overhaul is not
really applicable to ELT, see * in § C’) by means of an ELTA approved test and programming bench for
this occasion. This task must be performed by ELTA, an Approved ELTA service center or an ELTA
approved trained final operator.
Each battery pack is an assembly of two “D” LiMNO2 cells that include safety protections.
Refer to CMM 25-60-11 for details of operation.
NOTE: For CANADIAN applications, this information is summarized on the label stuck on the ELT
transmitter as presented here under.
Page 50
May 20/10
USER’S HANDBOOK
E. Discarding of Batteries
The batteries packs contain Lithium (LiMNO2) and must be discarded in compliance with the applicable
regulations in the country concerned.
NOTE :
The type of battery used is not dangerous for the environment provided that it is completely
discharged.
Contact ELTA for getting additional discarding information when necessary.
F. Test to be performed at the time of a ADT 406 S transmitter returns in workshop
Apply the following tests described in CMM 25-60-11 :
–
–
–
–
visual check
test of water sensor automatic activation
functional test of ADT 406 S ADT 406 S transmitter
RF test on the operational frequencies 121.5 – 243 – 406 MHz.
Page 51
May 20/10
USER’S HANDBOOK
44
6
5
3
7
2
8
1
10
9
11
12
13
1
2
3
4
5
6
7
8
9
10
11
12
13
14
– WHIP ANTENNA
– TX INDICATOR (red LED
– ARMED/OFF/ON GUARDED TOGGLE SWITCH
– TNC ANTENNA SOCKET
– ACTIVATION / IDENTIFICATION MODULE (Water sensor)
– BACK FACE
– METALIC STRAP
– VELCRO STRAP
– FLOAT ELEMENT
– FRONT FACE
– TEST PUSH BUTTON
– STANDARD MOUNTING BRACKET
– HOOP SWITCH GUARD
– POLYESTER LANYARD, under the ELT inside a location in 9
ELT ADT 406 S (P/N 01N65920) on standard mounting bracket (P/N 04N64250)
– Detailed Description
Figure 8
Page 52
May 20/10
USER’S HANDBOOK
5
6
7
4
3
8
2
1
9
13
10
11
12
1
2
3
4
5
6
7
8
9
10
11
12
13
14
– WHIP ANTENNA
– TX INDICATOR (red LED
– ARMED/OFF/ON GUARDED TOGGLE SWITCH
– TNC ANTENNA SOCKET
– ACTIVATION / IDENTIFICATION MODULE (Water sensor)
– BACK FACE
– METALIC STRAP
– VELCRO STRAP
– FLOAT ELEMENT
– FRONT FACE
– TEST PUSH BUTTON
– STANDARD MOUNTING BRACKET
– HOOP SWITCH GUARD
– POLYESTER LANYARD, under the ELT inside a location in 9
ELT ADT 406 S (P/N 01N65920) on standard mounting bracket (P/N 07N62351)
– Detailed Description
Figure 9
Page 53
May 20/10
COSPAS-SARSAT
TYPE APPROVAL CERTIFICATE
ETSO 2C91a AND ETSO 2C126
APPROVAL
Appendix A page 1
May 20/10
Appendix A page 2
May 20/10
TSO C91a AND TSO C126
APPROVAL
Appendix A page 3
May 20/10
Appendix A page 4
May 20/10
LOG BOOK
FACTORY SETTING
NEXT BATTERY SERVICING
……../……………. (MM/YYYY)
Appendix B page 1
May 20/10
FACTORY SETTING
Appendix B page 2
May 20/10
ENCODING UPDATE FORM
REGISTRATION COUNTRY:
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C OP-DESIGNATOR + S/N
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
CONTACT (PHONE, email…):
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
SIGNATURE AND STAMP:
NOTE : Attach the encoding update sheet issued from the ELTA encoding tool.
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 3
May 20/10
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 4
May 20/10
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 5
May 20/10
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 6
May 20/10
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 7
May 20/10
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
PROTOCOL:
ELT SERIAL NUMBER:
ELT S/N
A/C 24 Bit Address
A/C REG. MARK
TEST
C/S 15 HEX:
SIMPLIFIED DEC:
A/C MSN:
A/C OR A/P TYPE:
FINAL OPERATOR:
ISSUED BY:
DATE: ……/……/…………
(MM/DD/YYYY)
Appendix B page 8
May 20/10
MAINTENANCE TASKS
FINAL OPERATOR:
TYPE OF MAINTENANCE:
BATTERY SERVICING
INSPECTION
REPAIR
INSPECTION
REPAIR
RF TEST
TASK DESCRIPTION:
NEXT BATTERY SERVICING: ……/…………
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
NOTE : Attach the RF test sheet issued from the ELTA test tool.
FINAL OPERATOR:
BATTERY SERVICING
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
Appendix B page 9
May 20/10
MAINTENANCE TASKS
FINAL OPERATOR:
BATTERY SERVICING
INSPECTION
REPAIR
INSPECTION
REPAIR
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
FINAL OPERATOR:
BATTERY SERVICING
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
Appendix B page 10
May 20/10
MAINTENANCE TASKS
FINAL OPERATOR:
BATTERY SERVICING
INSPECTION
REPAIR
INSPECTION
REPAIR
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
FINAL OPERATOR:
BATTERY SERVICING
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
Appendix B page 11
May 20/10
MAINTENANCE TASKS
FINAL OPERATOR:
BATTERY SERVICING
INSPECTION
REPAIR
INSPECTION
REPAIR
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
FINAL OPERATOR:
BATTERY SERVICING
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
Appendix B page 12
May 20/10
MAINTENANCE TASKS
FINAL OPERATOR:
BATTERY SERVICING
INSPECTION
REPAIR
INSPECTION
REPAIR
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
FINAL OPERATOR:
BATTERY SERVICING
RF TEST
TASK DESCRIPTION:
DATE: ……/……/…………
(MM/YYYY)
(MM/DD/YYYY)
REPAIR STATION:
Appendix B page 13
May 20/10

04E66260C_USER`S HANDBOOK adt 406 S_rev-C

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