ACR Electronics SLB406 ELT SUPPORT MANUAL

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DESCRIPTION, OPERATION, INSTALLATION AND
MAINTENANCE MANUAL
FOR THE SLB 406 ELT
570-6700 Rev. B
This manual includes data for the equipment that follows:
Component Part No. Model No.
ARTEX PRODUCTS / ACR ELECTRONICS, INC
5757 Ravenswood Rd, Ft. Lauderdale, FL 33312
Cage Code: 60253
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
PROPRIETARY INFORMATION
This document contains proprietary information and such information may not be disclosed to others for any purpose, nor used for manufacturing purposes without written permission from ACR Electronics.
Information in this manual is subject to change without notice. ACR Electronics makes no warranty, expressed or implied, with regard to this manual, including but not limited to any implied warranties of merchantability, fitness for a particular purpose, and non-infringement. In addition, ACR Electronics makes no warranty with regard to the documentation or data contained herein. ACR Electronics is not liable in the event of incidentals, special, consequential, or any other damages in connection with or arising from furnishing, performance, or use of this manual.
Reproduction of this publication or any portion thereof by any means is prohibited. For further information contact Sales, ACR Electronics, 5757 Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (954) 981-3333
AIRWORTHINESS LIMITATIONS
The Airworthiness limitations section is FAA approved and specifies inspections and other
maintenance required under 14 CFR§ 43.16 and 91.403, unless an alternative program has been
approved.
IMPORTANT NOTICE
ACR Electronics will be responsible for full distribution and revisions of ICA’s (Instructions for
Continued Airworthiness). For inquiries regarding the content and currency of this manual,
contact ACR Electronics, 5757 Ravenswood Rd, Fort Lauderdale, FL 33312.
Telephone (954) 981-3333
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REVISION
CHANGE
DATE
REVISION
CHANGE
DATE
-
RELEASE
Dec 19/2006
- DCN 3078
Oct 02/2007
A
ECO 14756
Jul 29/2011
B ECO 15020
Mar 27/2012
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
RECORD OF REVISIONS
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SERVICE
BULLETIN
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ISSUE
DATE
SUBJECT
MANUAL
REV NO
MANUAL
REV DATE
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
SERVICE BULLETIN LIST
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Title Page
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Proprietary Information
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Record of Revisions
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Service Bulletin List
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List of Effective Pages
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Table of Contents
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Notices
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Introduction
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Description
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Operation
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Installation
20-24
Mar 27/12 Maintenance
25-33
Mar 27/12
Specifications
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Index
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LIST OF EFFECTIVE PAGES
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
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TABLE OF CONTENTS
PROPRIETARY INFORMATION ............................................. 2
RECORD OF REVISIONS ............................................................ 3
SERVICE BULLETIN LIST ...................................................... 4
LIST OF EFFECTIVE PAGE ...................................................... 6
RECORD OF REVISIONS ........................................................ 6
Notices .................................................................................. 9
Warnings ............................................................................... 9
Introduction ........................................................................ 10
Application ................................................................................................ 10
Description .......................................................................... 11
Certification:.............................................................................................. 12
Other requirements ................................................................................ 12
Programming: ........................................................................................ 12
Cospas-Sarsat Overview ............................................................................. 13
Figure 2 - SLB 406 View .......................................................................... 14
Operation ............................................................................ 15
Introduction ........................................................................................... 15
Deployment ........................................................................................... 15
Figure 3 – ELT Deployment ..................................................................... 15
Figure 4 - Indicators and Buttons ............................................................ 16
Functions .................................................................................................. 17
Activation .............................................................................................. 17
Normal Operation ................................................................................... 18
406.028 MHz Transmission ..................................................................... 18
121.5 MHz Homing Transmissions ........................................................... 18
Deactivation ........................................................................................... 18
Self-Test ................................................................................................ 18
Installation .......................................................................... 20
TSO C126 Paragraph D Requirements: ........................................................ 20
Parts List: .................................................................................................. 20
FAA Form 337 ........................................................................................... 21
Radio Station License ................................................................................. 21
Registration ............................................................................................... 21
International Beacon Registration Database ................................................ 24
Maintenance ........................................................................ 25
Periodic maintenance ................................................................................. 25
Battery replacement ............................................................................... 26
Figure 6 - ELT Battery Installation/Removal Exploded View ....................... 26
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Verification of Digital Message ................................................................. 28
Perform Transmitter Tests (Self Test) ...................................................... 29
Figure 7 - Test Button and LED Indicators ............................................... 29
Lanyard Deployment Test ....................................................................... 31
Figure 8 – Lanyard Deployment Test ....................................................... 31
Logbook Entry ........................................................................................ 33
Verify Registration .................................................................................. 33
Specifications ...................................................................... 34
Summary of Minimum Requirements ........................................................... 35
Operating Frequencies ............................................................................ 35
Output Power ......................................................................................... 35
Activation .............................................................................................. 35
Temperature .......................................................................................... 35
Fire Resistance ....................................................................................... 35
Input Power ........................................................................................... 35
Mechanical Characteristics ...................................................................... 35
Electrical Characteristics ......................................................................... 36
Software ................................................................................................ 36
Other Specifications ................................................................................ 36
Weight Table ............................................................................................. 37
Electrical Load Analysis (Current Draw) Table .............................................. 37
452-0129 Battery Pack ............................................................................... 38
182-0250 Auto Activation Lanyard .............................................................. 39
SLB 406 Overall Dimensions ....................................................................... 40
SLB 406 Series DO-160D Environmental Qualification Form .......................... 41
INDEX ....................................................................................................... 42
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Notices
1. Information contained in this manual is subject to regular updates and changes. Users under multi-unit contracts will be notified of these updates and changes as
they occur.
2. Complying with all applicable copyright laws is the responsibility of the user. Without
limiting the rights under copyright, no part of this document may be reproduced, stored in a retrieval system, or transmitted in any form or by any means including but not limited to, electronic, mechanical, photocopying, recording, or otherwise, or for any purpose, without the written permission of Artex Products / ACR Electronics, Inc. (hereafter Artex). This written permission shall be granted to military services and/or government agencies as part of a multi-unit contract.
3. Artex may have patents, patent applications, trademarks, copyrights, or other
intellectual property rights covering subject matter in this document. Except as expressly provided in any written license agreement from Artex, the furnishing of this document does not provide license to these patents, trademarks, copyrights, or other intellectual property.
Warnings
1. Never short-circuit the unit battery.
2. Do not expose this beacon to temperatures >85° C for a prolonged period -
overheating of the lithium battery of the unit causes a pressure increase and a risk of bursting and explosion.
3. Lithium batteries are classified as hazardous goods, appropriate precautions must be
taken when transporting beacons and battery packs.
4. The SLB 406 should be activated only in an actual emergency situation, because its
activation triggers a search and rescue operation.
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Introduction
This manual contains all necessary information to describe, operate, install and maintain the SLB 406 ELT. The manual contains all necessary information to ensure continued airworthiness. Artex does not generate Aircraft Flight Manuals (AFM) or supplements thereof; these documents are the responsibility of the aircraft operator as required by FAR 121 subpart G §121.131 through §121.141.
Information presented in this manual is accurate at time of printing but is subject to change. Refer to the ACR products web site at www.acrartex.com for the latest information and any updates to this manual.
Web links provided in this manual were accurate at time of printing but are subject to change.
Regulatory references are aimed at FAA requirements. Consult your national aviation authority for requirements if you are located outside of the US.
Application
This manual constitutes FAA approved data as described in AC 43.9-1E, paragraph (h)(2) and AC 43-210, chapter 2, paragraph 201(a)(6) for major alterations. Not all installations are “major”; consult an FAA designee or regional office for clarification.
The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install this article either on a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. The article may be installed only if further evaluation by the applicant documents an acceptable installation and it is approved by the Administrator.
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Description
The SLB 406 (Survivor Locator Beacon) is a Type S (Survival) Emergency Locator Transmitter that provides world-wide alerting in emergency situations via a network of satellites of the Cospas-Sarsat distress alerting system. This system enables the location, nationality, unit serial number, and user specific registration data of the personal locator beacon to be immediately identified with the receipt of the alert.
The SLB 406 was developed to meet demanding environmental standards for individual’s
onboard aircraft, on land and at sea. The beacon is made of tough poly-carbonate plastic, and is designed to withstand the rigors of severe outdoor use. The flip face cover (see Figure 4) protects the buttons and indicators against damage and inadvertent activation. It is fully waterproof to 10m, operable over the -20°C to +55°C temperature range. This ensures that should a survivor need help, the message will get through.
The SLB 406 user interface is intuitive and easy to use, no matter the condition of the survivor. The SLB 406 can be used equally well with either the right or left hand, with buttons large enough to be operated while wearing gloves. Activating the beacon is simple and can be done with one hand, or can be activated automatically upon life vest inflation. For manual activation, the survivor simply flips open the face cover and presses the activate button, which immediately activates the beacon. Visual indications of beacon activation is provided. The beacon can be switched off by the rescue crew after the survivors have been rescued or by the survivors if multiple beacons are active. A beacon that has been turned off can be reactivated simply by pressing the activate button. The safety lanyard can be attached to the user’s equipment to ensure that the beacon is not lost or otherwise separated from the person in distress.
Examples of the information that can be contained in that message are shown below:
Serial Number of the transmitter or Aircraft ID (24-Bit Address or Tail Number) Country Code Cospas/Sarsat ID Code (Serialized Only)
The 406.028 MHz transmitter with the supplied battery will operate for 24 hours, and then shut down automatically. The 121.5 MHz transmitter will continue to operate until the unit has exhausted the battery power which will be greater than 50 hours.
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Certification:
The SLB 406 has been certified to the following:
TSO C126 TSO C91a in the 121.5/406 MHz configuration as referenced in TSO-C126,
paragraph (e).
FAR Part 91 – mandatory automatic ELT requirements Cospas-Sarsat T.001, Type Approval Certificate #148 47 CFR Part 87 (FCC requirements) Note: Per FCC regulations 47 CFR § 2.902, the
ELT is tested per “Verification” method, the FCC does not issue certificates for ELT’s.
The FCC identifier grantee code for Artex is H4K.
Other requirements
The SLB 406 was not tested for other specifications beyond the requirements of TSO C126. Compliance with additional FAR’s (such as FAR 25) are the responsibility of the installer as required for installation approval.
The US Federal Aviation Regulations (FAR’s) are available at:
http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf/MainFrame?Op enFrameSet
NOTE: For use outside of the US, contact your local civil aviation authority for ELT requirements.
Programming:
The SLB 406 supports the following Protocols:
Aviation ELT / Tail Number (Short) Serial User/ Aircraft 24 Bit Addr (Short) Serial User / Aircraft 24 Bit / National (Short) Serial User / ELT / COSPAS (Short) Serial User / ELT / National USA (Short) Serial User / Aircraft Operator (Short)
For a complete discussion of ELT programming protocols please see Cospas-Sarsat Documents G.005 and T.001 available at www.cospas-sarsat.org.
The United States accepts all of the above listed protocols. For use outside of the US, contact your local civil aviation authority for accepted or required programming protocols. The desired protocol must be provided to Artex at time of ordering.
NOTE: The SLB 406 is not currently configured for use with Location Protocols.
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Cospas-Sarsat Overview
Cospas-Sarsat is an international, humanitarian search and rescue system that uses satellites to detect and locate emergency beacons carried by ships, aircraft, and individuals. The system consists of a network of satellites, ground stations, mission control centers, and rescue coordination centers.
When a 406 MHz emergency beacon is activated, the signal is received by a satellite and relayed to the nearest available ground station. The ground station, called a Local User Terminal (LUT), processes the signal and calculates the position from which it originated using the Doppler Shift process. This position is transmitted to a mission control center (MCC) where it is joined with identification data and other information on that beacon.
The MCC then transmits an alert message to the appropriate rescue coordination center based on the geographic location of the beacon. If the location of the beacon is in another country's area of responsibility, then the alert is transmitted to that country's assigned MCC.
On average, from the time a 406 MHz emergency beacon is activated it takes 8-10 minutes for the alert message and accompanying identification data to arrive at the appropriate rescue coordination center. The Cospas-Sarsat system provides the capability for protecting lives. With a 406 MHz beacon, a distress message can be sent to the appropriate authorities from anywhere on Earth 24 hours a day, 365 days a year.
Figure 1 Cospas-Sarsat Overview
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Figure 2 - SLB 406 View
SLB 406 ELT
Warning:
The ELT is NOT buoyant, and must be attached to a
floatation device when in water environments.
Failure to observe this warning may cause the ELT to fail when it is critical for it to operate. Such failure may cause
loss of life.
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Operation
Introduction
The SLB 406 is designed to provide world-wide alerting in emergency situations via the Cospas-Sarsat System. The SLB 406 operates on two frequencies simultaneously – 406 MHz as the alerting frequency for the Cospas-Sarsat satellite system, 121.5 MHz as the civilian homing frequency to aid SAR responders. Following is a description of the operating instructions and functions of the SLB 406.
Deployment
In the storage configuration, the antenna is wrapped around the chassis of the ELT and held in place with a snap on the Activation Lanyard. To deploy the antenna, simply unsnap and pull away from the Activation Lanyard. The antenna may be rotated for best position. The SLB 406 will provide the best transmission characteristics when it is placed on a flat surface with the antenna oriented vertically.
The SLB 406 can also be held in the hand with the antenna oriented vertically. See Figure 3 below:
Figure 3 – ELT Deployment
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Indicators and Buttons
Figure 4 displays the functional buttons and LED indicators on the faceplate of the SLB
406.
Figure 4 - Indicators and Buttons
ACTIVATE: Press and hold for approximately 2 seconds to activate the beacon.
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THIS TRANSMITTER IS AUTHORIZED FOR USE ONLY DURING SITUATIONS OF GRAVE AND IMMINENT DANGER, WHEN ALL OTHER MEANS OF SELF RESCUE HAVE BEEN EXHAUSTED.
OFF: Press for approximately 2 seconds to turn SLB off. TEST: Press for approximately 2 seconds to initiate Self Test operations. XMIT: LED flashes Red once every two seconds indicating Normal Operation.
During an actual 406 MHz transmission (nominally every 50 seconds), the LED stays Red for the full 406 MHz pulse transmission –approximately one second.
PASS: LED flashes green for 60 seconds indicating a successful Self Test operation.
FAIL: LED flashes red for 60 seconds indicating a failed Self Test operation.
Functions
Activation
The SLB 406 can be activated in two modes: 1) Automatic Activation, and 2) Manual Activation. The Automatic Activation mode requires the use of the automatic activation lanyard/Activation Lanyard attached to a life raft or the inflatable portion of a life vest. In this mode the beacon will be automatically activated upon life vest/raft inflation without any user action. Beacon activation occurs when the activation lanyard is separated from the beacon. When the beacon is activated, the red XMIT LED will illuminate for approximately one second to acknowledge. To activate the SLB 406 in the Manual Activation mode, press the ACTIVATE button for approximately two seconds until the red XMIT light illuminates. When the beacon is activated, the red XMIT LED will illuminate for approximately one second to acknowledge. Figure 5 shows the protective faceplate of the SLB 406 which protects the buttons from inadvertent activation or turnoff.
Figure 5 – Protective Face Plate
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Normal Operation
After this initial Activate illumination, the red XMIT LED will blink every two seconds.
406.028 MHz Transmission
The 406.028 MHz transmission occurs approximately once every 50 seconds. This transmission includes coded information including the beacon’s unique ID. During the transmission, the red XMIT LED lights for the duration of the transmit pulse. There is a 50 second delay in the initial transmission after activation as required by Cospas-Sarsat. The purpose of this delay is to minimize the occurrence of false alerts, as a person has 50 seconds to turn off a beacon that was mistakenly activated.
121.5 MHz Homing Transmissions
These homing transmissions operate continuously while the beacon is activated except during the 406 MHz pulse transmissions.
Deactivation
The SLB 406 can be deactivated from either the Automatic or Manual Activation modes by pressing and holding the OFF button for approximately two seconds. The red XMIT LED will illuminate for 1 second prior to turning off to acknowledge the deactivation. The red XMIT LED will stop blinking when the beacon is turned off. The SLB 406 can be turned back on by simply pressing the ACTIVATE button for approximately two seconds.
If the beacon is deactivated without the Activation Lanyard installed, the batteries will continue to discharge.
Self-Test
Self Tests are to be conducted only by second line maintenance
To conduct a self-test of the SLB 406, press the TEST button and hold for approximately two seconds. The red XMIT LED will illuminate for approximately one second to acknowledge.
The PASS LED (green) and the FAIL LED (red) will then illuminate together for approximately 1 second to test these LEDs.
During the self-test process, the XMIT LED flashes in the following progression:
The XMIT LED illuminates solidly for approximately 1 second during the 406.028 MHz and 121.5 MHz pulse tests.
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The XMIT LEDs flashes simultaneously for approximately 1.5 seconds during the
121.5MHz modulation test.
Following the test the PASS LED will flash at a rate of twice per second for a total period of 60 seconds to indicate that the SLB 406 is fully functional. Alternatively, the FAIL LED will flash at a rate of twice per second for a total period of 60 seconds to indicate that the SLB 406 has malfunctioned. The unit then shuts off.
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Installation
The ELT intended application is to be installed as part of a slide raft emergency system used in commercial aircraft or other life raft application. Design of the ELT was based on the assumption that the ELT would be inserted in a pocket in the raft. For automatic activation, connect the Auto Activation Lanyard (as shown on page 39) to the raft such that inflation of the raft will pull the Lanyard from the ELT.
Note: Installation of an Automatic Fixed “Type AF” ELT may also be required; contact you local Flight Standards District Office (or applicable civil aviation authority representative) if in doubt.
TSO C126 Paragraph D Requirements:
“The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install this article on a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. The article may be installed only if further evaluation by the applicant documents an acceptable installation and it is approved by the administrator.”
Note: Aircraft manufacturers may also have guidance on ELT installation; refer to and follow any applicable Type Approval or STC data for your aircraft. If located outside of the US, follow all applicable regulations for your national authority.
Parts List:
Included in standard kit:
The SLB 406 is offered as a complete kit. Please review the components included in a base kit. The following parts should be included. Contact Artex Aircraft Supplies if shortages are found.
ELT P/N 453-6700 (completely assembled, includes Battery Pack, Antenna, Safety
Lanyard and Activation Lanyard)
Battery Pack, Artex P/N 452-0129 (Li/SO2) (included with ELT above) Screw, 6-32 x ¾, Socket SS, Artex P/N 209-0001 (included with ELT above, used to
attach Battery Pack)
Activation Lanyard, Artex P/N 182-0250 (included with ELT above) Manual, Artex P/N 570-6700 – also available free for download at www.acrartex.com
All of the above listed parts (except Antenna and Safety Lanyard) may be purchased separately as line replaceable parts. Contact Artex at 1-800-432-0227 for details, pricing and availability.
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Note: Removal of the Antenna is not permitted; unit must be return to Artex for repair or replacement of the antenna.
FAA Form 337
For installations that are considered a “major alteration”, an FAA Form 337 will be
required. Information regarding the completion of Form 337 can be found in Advisory Circular AC 43.9-1E. This Manual constitutes FAA approved data as described in AC
43.9-1E, paragraph (h)(2) and AC 43-210, chapter 2, paragraph 201(a)(6) for major
alterations. Not all installations are “major”; consult an FAA designee or regional office for clarification. Generally, the installation of the SLB 406 will not require a Form 337 but contact you local Flight Standards District Office if in doubt.
Radio Station License
A Radio Station License is not required by the FCC for Emergency Locator Transmitters (ELTs). See the FCC web site at http://wireless.fcc.gov/aviation/fctsht4.html which states:
On October 26, 1996, the FCC released a Report and Order in WT Docket No. 96-82, FCC 96-421 eliminating the individual licensing requirement for all aircraft operating domestically. This means that you do not need a license to operate a two-way VHF radio, radar, or ELT aboard aircraft operating domestically. All other aircraft radio stations must be licensed by the FCC either individually or by fleet.
FCC Form 605 which replaced FCC Form 404 in 1999 is not required for ELTs.
For more information, contact the FCC at:
Federal Communications Commission
445 12th Street SW
Washington, DC 20554
1-888-CALL-FCC (1-888-225-5322)
E-mail: fccinfo@fcc.gov
For radio station license information outside of the Unites States, contact you national radio communications authority for assistance.
Registration
REGISTRATION FORMS (OR LINKS TO THEM ) ARE PROVIDED ON THE ARTEX WEB SITE AT www.acrartex.com .
When a 406 MHz ELT is installed in an aircraft, it is imperative that the aircraft owner register the ELT. In the United States the National Oceanic and Atmospheric Administration (NOAA) is the registration agency. Each 406 MHz ELT contains a unique identification code that is transmitted to the satellite. This helps the “Rescue
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Coordination Center” (RCC) determine whether an emergency actually has occurred. The
unique identification permits accessing a data base. In the United States the data base contains the following:
Owner’s Name
Address
Telephone Number
Aircraft Type
Aircraft Registration Number
This data facilitates inquiries as to the whereabouts of the aircraft, the existence of a flight plan and so forth. The above information should be kept up to date, with any changes to the data corrected (i.e. change of address, phone numbers, etc.).
Important Notice -
The information you furnish is mandatory and is intended to assist search and rescue teams in locating you or your craft in the event of beacon activation. The information will be provided to the United States Coast Guard, United States Air Force, and other Search and Rescue (SAR) teams as appropriate in the event of beacon activation. It will also be used to conserve SAR resources by helping to eliminate false alert deployments, e.g. an inadvertent activation can be resolved with a phone call.
Failure to register, re-register (which occurs every two years) or to notify NOAA of a change in the status for a 406 MHz beacon could result in penalties and/or fines being issued to the owner. An owner is required to notify NOAA of any changes to the registration information. Please note, due to the critical need for up-to-date registration information, NOAA will update the database accordingly if a beacon owner’s registration has expired and credible information is provided from SAR sources. NOAA will also seek information from other databases to update and/or complement the existing information for a beacon registration. Solicitation of this information is authorized by Parts 80, 87, and 95 of Title 47 of the U.S. Code of Federal Regulations (CFRs).
Please Read Before Completing Registration
There is no charge for beacon registration. This is a service provided by the U.S. Government.
All online registrations will be entered into the National 406 MHz Beacon Registration Database on the same day of entry. Registration forms received via the postal mail service will be entered into the National 406 MHz Beacon Registration Database within 2 business days of receipt. For online registrations, a letter with an attached registration information sheet will be sent immediately via e-mail or fax (if provided), or via postal mail within two weeks. Once your registration confirmation is received, please review all information. Any changes or updates to your registration information can be done via the internet, fax, e-mail or postal mail. If you do not receive your registration
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confirmation from NOAA on the same day you submit it over the internet or within two weeks if you submit it by postal mail, please call NOAA toll-free at:
1-888-212-SAVE (7283) or 301-457-5678 for assistance.
After initial registration (or re-registration) you will receive a NOAA Proof of Registration Decal by postal mail. It is required that you affix the registration decal to your beacon. If for some reason you do not receive the registration decal within two weeks, please call NOAA at the above number for assistance. Registration forms can be found on the NOAA SARSAT website at: www.sarsat.noaa.gov or at:
www.beaconregistration.noaa.gov.
Although the information provided will become a matter of public record, there is no intent to circulate the data furnished beyond its intended purpose, i.e., to assist SAR forces in carrying out their mission of rescue assistance and false alert abatement. Public reporting burden for the collection of this information is estimated to average 15 minutes per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden should be sent to:
SARSAT Beacon Registration NOAA
NSOF, E/SP053 4231 Suitland Road Suitland, MD 20746
Or call: 1-888-212-SAVE (7283) or 301-457-5678
WARNING: If the ELT is moved to a different aircraft than which it was originally registered with, the ELT must be re-registered and the product label re-marked to indicate the new programming and/or new country of registry.
NOTICE: FOR ELTS THAT WILL HAVE A COUNTRY OF REGISTRATION OTHER THAN USA, PLEASE CONTACT THE APPROPRIATE CIVIL AVIATION AUTHORITY IN THAT COUNTRY FOR GUIDELINES AND DOCUMENTATION NEEDED TO ASSURE PROPER REGISTRATION
Refer to Cospas/Sarsat Documents G.005 and S.007 for information regarding ELT programming and registration, available at www.cospas-sarsat.org.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
International Beacon Registration Database
Effective January 16, 2006, Cospas-Sarsat implemented an International Beacon Registration Database (IBRD) to allow 406 MHz beacon owners the ability to register their beacon where no national registration database exists via the internet at
www.406registration.com. There is no charge for this service.
Beacons registered with the IRBD must conform to any national regulations regarding their beacon where no national registration database exists via the internet at
www.406registration.com. There is no charge for this service.
Beacons registered with the IRBD must conform to any national regulations regarding ELT programming. Cospas-Sarsat does not provide guidance on the specific coding options that are accepted by individual national authorities or administrations.
The IRBD cannot accept registrations for countries that have informed Cospas-Sarsat that they operate national registries.
The minimum information required to register a beacon in the IBRD is:
Beacon Hexadecimal ID Owner name and phone number Emergency contact name and phone number Vehicle Type (Selectable from a menu) Vehicle Name, MMSI, Call sign or identification number
Links to all referenced web sites are available at www.acrartex.com.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Maintenance
This section describes minimum continued airworthiness requirements that can be performed by the aircraft owner/operator. Additional maintenance must be performed by an authorized Artex Repair Station.
Periodic maintenance
In the United States, minimum maintenance requirements for ELTs are stated in FAR
91.207 paragraph (d):
(d) Each emergency locator transmitter required by paragraph (a) of this section must be inspected within 12 calendar months after the last inspection for-­(1) Proper installation; (2) Battery corrosion; (3) Operation of the controls and crash sensor; and (4) The presence of a sufficient signal radiated from its antenna.
To ensure continued reliability and airworthiness, your ELT must be inspected for damage and wear caused by age, exposed elements, vibration, etc. Inspections are also to take place annually per FAR Part 91.409. FAR 43, Appendix D(i) states in part that each person performing an annual or 100-hour inspection shall inspect the following components of (the ELT):
(1) (ELT unit and mount) for improper installation and insecure mounting.
(2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects.
(3) Bonding and shielding - for improper installation and poor condition.
(4) Antenna, including trailing antenna-for poor condition, insecure mounting, and improper operation.
NOTE: All references to maintenance requirements for the United States shall also apply to all ELT users outside of the US unless otherwise required by the installer / aircraft maintenance procedures or the relevant national regulations.
NOTE:
All references to test equipment are generic; Artex makes no specific equipment references (by manufacturer, etc). All tests described herein must be performed by qualified personnel that are familiar with test equipment as well as the specifications and parameters described.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Battery replacement
To remove battery, perform the following steps:
1) Remove SLB 406 from storage
2) Unfasten the Antenna from the Velcro on the Activation Lanyard
3) Remove the 4 x 6-32 hex head cap screws that attach the top Transmitter Assembly
to the Battery Pack
4) Disconnect Battery connector (this is a very short harness)
Verify the battery expiration date. If the battery pack has not expired it may be reinstalled. The battery pack must be replaced with a new one:
After use in an emergency When the transmitter has been in use for more than 1 cumulative hour After an inadvertent activation of unknown duration On or before the battery replacement (expiration) date
To re-install or replace the Battery Pack perform the following steps:
1) Plug in Battery connector to bottom of Transmitter Assembly
2) Assemble Battery Pack to Transmitter Assembly using the 4 x 6-32 hex head cap
screws, evenly torque to 9 in lbs (1 Nm)
3) Wrap Antenna around Battery Pack and snap into place and position onto Velcro
patch that is on the Activation Lanyard
Note: Replacement battery packs are provided with a fresh gasket, be sure to discard the old gasket with the old battery pack if replacing the battery pack.
APPROVED BATTERIES AVAILABLE FROM ARTEX OR ANY ARTEX DEALER, OR:
ACR Electronics, Inc
5757 Ravenswood Rd
Fort Lauderdale, FL 33312
(954) 981-3333, FAX (954) 983-5087
web site: www.acrartex.com
Figure 6 - ELT Battery Installation/Removal Exploded View
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
Verification of Digital Message
SLB 406 ELT
NOTE:
This test is not mandatory per FAR 91.207(d) however Artex strongly
recommends that it be performed as part of annual maintenance.
Verify the 406 MHz digital message using a test set capable of receiving and decoding the message. Artex suggests the ELT Test Set (ETS) P/N 453-1000. Contact your local Artex dealer for availability of the ETS or call Artex direct at 1-800-432-0227. Other beacon testers can be used for the digital message verification. Follow instructions provided with the test set.
Realize that the ARTEX 406 MHz ELT transmits a 406 MHz message upon reset, which is encoded such that it will be ignored by the SAR satellite system. This 15-digit number is used to register the ELT with the appropriate 406 MHz ELT registration authority. In the US, the National Oceanic and Atmospheric Administration (NOAA) maintains the database of registered ELT’s.
To verify the digital message, perform the following steps:
1. Perform all necessary steps to prepare Test Set to receive 406 MHz signal including (but not limited to) turning on power, activating program or any other steps required for the particular Test Set being used.
2. Perform the Installed Transmitter Test “self test” as described on page 29.
3. Watch the screen on the Test Set to ensure that a message has been received. Repeat “self test” if necessary.
4. View message, ensure that all applicable information is correct (country code, aircraft ID, etc.).
5. The 15 digit ID hex ID (for example “ADC6492640D3411F”) should match what is shown on the ELT product label. This is the 15 digit hex ID (Unique Identification Number or “UIN”) that is used to register the ELT.
The test message contains all the information contained in the actual distress message except position data and there is a special digital test prefix that tells the COSPAS/SARSAT satellites to ignore the message.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Perform Transmitter Tests (Self Test)
Self tests must be performed outside of metallic enclosures and at least 2 meters away from large metallic surfaces which may reflect electromagnetic waves. If restrictions are not observed it is possible that self test may report failure when the beacon is operating properly.
Following are step-by-step instructions for performing the field tests.
1) Examine the SLB 406 closely for signs of physical damage including cracked or punctured housing, cracked or broken face plate or damaged antenna.
Note: The antenna is not intended to be removed from the ELT by the user.
2) Perform Self-test by pressing the self-test button (see Figure 7) for two seconds, then releasing the button.
3) Observe the red XMIT LED. It will light up for one second as acknowledgement.
4) The Pass LED and the Fail LED will then light up together for one second. After this, at different stages of the test, the other LEDs glow steadily or flash depending on the particular self-test being performed.
5) Check for Pass/ Fail. After five seconds, either the ‘Pass’ or the ‘Fail’ LED will start flashing for sixty seconds, the green LED for pass and the red LED for fail.
Figure 7 - Test Button and LED Indicators
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
The unit will shut off automatically at the end of self-test. If the self-test passes (that is the green PASS LED flashes for 60 seconds) no further tests are required.
If the self-test fails (the red FAIL LED flashes), further investigation is necessary. The unit should be returned to Artex for inspection and corrective action.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Lanyard Deployment Test
This test ensures that the beacon will activate when the lanyard Activation Lanyard is removed. The tests should be performed with a fully assembled beacon.
Pull out the Activation Lanyard from the SLB 406 unit. Observe that the unit is activated by this operation by observing the XMIT LED begins to flash. Deactivate the unit by re­installing the Activation Lanyard. (Push it back in place), and observing that the XMIT LED ceases to flash.
The beacon will not begin to transmit for 50 seconds after activation, so this test can be completed outside the shielded box as long as the Activation Lanyard is re-inserted within 50 seconds of removal.
Figure 8 – Lanyard Deployment Test
1) Secure the beacon against a secure surface (such as a wall).
2) Using the Pull force gauge in tension mode and on PEAK setting.
3) Apply pressure to tension the lanyard.
4) Pull lanyard with a quick pull action, see Figure 8 above.
5) Deactivate the unit by re-installing the Activation Lanyard (Push it back in place).
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
Min
Nom
Max
Removal force
2.25 kg
5.4 kg
6.4 kg
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
6) Note the pull out force from the gauge. Verify pull force is within the range shown in the table below.
7) The beacon will not begin to transmit for 50 seconds after activation, so this test can be completed outside the shielded box as long as the activation lanyard is re-inserted within 50 seconds of removal.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
NOTE: All ELT “ON” tests should be performed within the first five minutes after the hour UTC or as required by local or national authorities.
Always perform the tests within the first 5 minutes of the hour. Notify any nearby control tower of your intensions, in accordance with AC 43.13-1B, Section 12-22, Note 3. If outside of the US, always follow all local or national regulations for testing of ELTs.
Logbook Entry
Enter the date the test technician’s initials and whether the ELT passed or failed into the aircraft’s logbook.
Verify Registration
Check ELT for signs of registration. In the US, NOAA supplies a beacon registration label that is applied to the ELT when it is registered. The following address should be used to register and obtain information on how to register 406 MHz ELT’s in the United States:
SARSAT Beacon Registration NOAA
NSOF, E/SP053 4231 Suitland Road Suitland, MD 20746
http://www.sarsat.noaa.gov/
Or call (888) 212-SAVE (7283) or (301) 457-5678
The ACR Electronics Artex Products website also contains information on registering beacons in other countries:
www.acrartex.com
NOTICE: FOR ELTS THAT HAVE A COUNTRY OF REGISTRATION OTHER THAN THE USA. PLEASE CONTACT THE APPROPRIATE CIVIL AVIATION AUTHORITY IN THAT COUNTRY FOR GUIDELINES AND DOCUMENTATION NEEDED TO ASSURE PROPER REGISTRATION
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
COSPAS-SARSAT 406 MHz Beacon
Frequency
406.028 MHz
Power
5W ± 2 dB
Modulation
Phase modulation ± 1.1 Radians
Stability
Full compliance with COSPAS-SARSAT specification T.007
Homing Beacon
Frequency
121.5 MHz
Power
100 mW minimum
Modulation
Amplitude modulation, swept downwards between 1000 Hz and 300 Hz with a sweep rate of 3 Hz
Operational
Beacon Type
Type “S” (Survival) as defined per RTCA/DO-204 §2.1.15
Activation
One hand gloved operation, left or right
Endurance
24 hours at -20 ºC (406 MHz), 50 hours at -20 ºC (121.5 MHz)
Antenna
18 cm flexible
Controls
Activate, Off, Test
Indicators
Transmit, Test Pass, Test Fail
Environmental
Altitude
Up to 15,000 meters (50,000 feet)
Rapid decompression
Will survive at up to 15,000 meters (50,000 feet)
Depth
Waterproof to 1 meter (post crash immersion)
Operating Temperature
-20 C to +55 C
Humidity
95%
Maintenance
Battery Storage
5 Years nominal (refer to battery expiration label for exact date)
Built in Test
Functional test with pass/fail indicators
Battery Type
LiSO2
Storage Temperature
-55 C to +85 C
Construction
Material
Poly-carbonate high impact plastic with UV inhibitors
Color
Safety Yellow
Outside dimensions
176 mm x 90 mm x 55 mm
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
Specifications
SLB 406 ELT
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
Weight
737 g (including battery pack)
Volume
557 cm3
Design Specifications
RTCA DO-204 RTCA DO-183 COSPAS-SARSAT T.001
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Summary of Minimum Requirements
Operating Frequencies
406.028 MHz +/- 2 kHz Bi-phase L; Emission designator G1D 121.5 MHz +/-6.0 kHz AM; Emission designator A3X
Output Power
406 MHz: 37 dBm ± 2 dBm (3.16W Min to 7.94 W Max) (440 ms / 50 sec) PERP or
EIRP for 24 hours @ -20ºC to +55ºC
121.5 MHz: >/= 20.0 dBm (100mW) PERP for 50 hours or EIRP for 48 hours @ -20ºC
to +55ºC
Activation
Manual or Auto Activation Lanyard
Temperature
Storage: -55ºC to +85ºC
Operational: -20ºC to +55ºC
Fire Resistance
15 sec. flame per RTCA/DO-204 §2.3.7.1
Input Power
None
Mechanical Characteristics
Vibration: 10 G’s, 5Hz to 2000Hz
Shock: 50 G’s for 11 ms
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Humidity: 95% for 50 hours
Penetration: 55 LBS from 6 inches
Crush: 1,000 LBS
Electrical Characteristics
Spurious Emissions per CFR 47 Part 87 for 121.5 MHz; per RTCA/DO-204 for 406 MHz
Impedance: 50 ohms (nominal) at 121.5/406 MHz
Software
RTCA/DO-178B, Level D
Other Specifications
The SLB 406 was not tested for other specifications beyond the requirements of TSO C126. Compliance with additional FAR’s (such as FAR 25) are the responsibility of the installer as required for installation approval.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
PART NUMBER
DESCRIPTION
WEIGHT
453-6700
SLB 406 ELT
(complete w/ battery, antenna and auto activation lanyard)
1 LB 10 oz (737 g) Max
452-0129
Battery Pack
11.7 oz (332 g) Typ
182-0250
Auto activation lanyard
0.3 oz (8.5 g) Typ
Component
Aircraft Power
Continuous
5 Minutes
5 Seconds
ELT
0 A
0 A
0 A
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
Weight Table
*NOTE: The Antenna is integral with the ELT and is not intended to be removed and is not a line replaceable part. Replacement or repair of the Antenna may only be performed by Artex or by an Authorized Artex Repair Station.
Electrical Load Analysis (Current Draw) Table
Note: The SLB 406 does not connect or interface to aircraft power or any aircraft
electrical or data system.
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
452-0129 Battery Pack
Chemistry: Lithium-Sulfur Dioxide (Li/SO2)
Lithium metal content: 5.07 grams
Voltage: 9.0 VDC (open cell)
Amp-hour rating: 4.5 Ahrs
Certification: Cospas/Sarsat, DOT (T1-T8 testing for Class 9 Hazardous Goods) and
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
182-0250 Auto Activation Lanyard
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
SLB 406 Overall Dimensions
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
CATEGORY
SECTION
DESCRIPTION
D1
4.0
TEMPERATURE
ALTITUDE
X
4.5.4
IN FLIGHT LOSS OF
COOLING
B
5.0
TEMPERATURE
VARIATION
A
6.0
HUMIDITY
Per DO-204
7.0
SHOCK
Per DO-204
8.0
VIBRATION
X
9.0
EXPLOSION
PROOFNESS
R
10.0
WATERPROOFNESS
X
11.0
FLUIDS
SUSCEPTIBILITY
X
12.0
SAND & DUST
X
13.0
FUNGUS RESISTANCE
S
14.0
SALT SPRAY
X
15.0
MAGNETIC EFFECT
X
16.0
POWER INPUT
X
17.0
VOLTAGE SPIKE
X
18.0
AUDIO FREQUENCY
CONDUCTED
SUSCEPTIBILITY
A
19.0
INDUCED SIGNAL
SUSCEPTIBILITY
Per DO-204
20.0
RADIO FREQUENCY
SUSCEPTIBILITY
X
21.0
EMISSION OF RF
ENERGY
XXXX
22.0
LIGHTNING
X
23.0
LIGHTNING DIRECT
EFFECTS
X
24.0
ICING
X
25.0
ESD
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
SLB 406 Series DO-160D Environmental Qualification Form
Environmental Categories: D1XBA[204][204]XRXXXSXXXXA[204]X[XXXX]XXX
See RTCA/DO-160D, Appendix A for a complete explanation of Environmental Categories. References to “Per DO-204” are for tests performed in accordance with RTCA/DO-204.
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INDEX
A
Antenna, 6, 11 Application, 1
B
Battery pack, 26 Battery replacement, 16
C
Certification, 3 Cospas-Sarsat, 3, 13 Current Draw Table, 25
D
Description, 2 Dimensions, overall, 28 DO-160D, 29
F
FAA Form 337, 11 FCC Certification, 3 Frequencies, 23
I
IBRD, 13 Installation, 10 Introduction, 1
L
Lanyard, 27 Line replaceable parts, 10 Logbook entry, 21
M
Maintenance, 15
N
NOAA, 12, 13, 18
O
Operation, 6
P
Parts List, 10 Power, 23 Protocols, 3
Q
Qualification Test Form, 29
R
Radio Station License, 11
Registration requirements, 11, 14,
21
S
Safety Lanyard, 2 Self test, 19 Software, 24 Specifications, 22
T
Testing, minimum, 15 TSO, 1, 3 Type, 2, 22
W
Weight Table, 25
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Initial Issue DEC 19/2006
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ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
SLB 406 ELT
THIS IS A BLANK PAGE
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Initial Issue DEC 19/2006
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