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Information in this manual is subject to change without notice. Wulfsberg 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, Wulfsberg Electronics makes
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Reproduction of this publication or any portion thereof by any means is prohibited. for further information contact Sales, Wulfsberg Electronics, 6400 Wilkinson Drive, Prescott, Arizona, 86301. Telephone (928) 708-1550
(1)This manual describes the operation, installation, and maintenance of the Model C406-2
Series emergency locator transmitter (ELT). This information is provided to ensure initial and
continued airworthiness. Information presented in this manual is accurate at time of printing,
but is subject to change. Refer to the Artex web site at www.artex.net for the latest
information and any updates to this manual.
(2)Information on COSPAS-SARSAT emergency locator beacon registration requirements and
procedures is provided in Appendix A – ELT Registration, on page 81.
C406-2 (453-5000), C406-2HM (453-5001)
INTRODUCTION
(3)Web links provided in this manual were accurate at time of printing but may be subject to
change.
(4)Wulfsberg Electronics reserves the right to add approved components to the ELT system;
including, but not limited to antennas, remote switches, and coaxial cables.
(5)Regulatory references contained herein are generally confined to United States and Canadian
requirements and, in any case, should not be considered all encompassing. Consult your
national aviation authority for applicable requirements.
SUBTASK 25-62-11-990-002
B.Application
(1)This manual constitutes supporting data/documentation for the C406-2 Series ELT, including:
(a)Description and Operation
(b)Test and Fault Isolation (includes inspection criteria)
(c)Removal
(d)Installation
(e)Registration
(f)Illustrated Parts List
(2)In the United States, the C406-2 Series ELT must be installed and maintained in accordance
with the requirements herein and 14 CFR, FAR Parts 43, and 91; and other airworthiness
requirements, as applicable.
(3)In Canada, the C406-2 Series ELT must be installed and maintained in accordance with the
requirements herein and Canadian Aviation Regulations (CAR), Part V, Paragraph 551.104 and
other CAR airworthiness requirements, as applicable.
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
(4)C406-2 Series ELT installation and maintenance in all other countries must comply with the
requirements herein and applicable national airworthiness requirements.
(5)The accessories (i.e., remote switch and antennas) addressed in this manual are the
accessories most commonly associated with the C406-2 Series ELT. Other options, such as a
different remote switch configuration or an ELT/NAV Interface, should be installed and
maintained in accordance with the written instructions specific to the accessory.
NOTE
:Contact Wulfsberg Electronics for optional accessories approved for use with a C406-
2 Series ELT.
(6)To ensure proper operation, only parts listed in the Illustrated Parts List of this manual or
those recommended by Wulfsberg Electronics may be used as replacement parts for the
C406-2 Series ELT.
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COBHAM AVIONICS WULFSBERG ELECTRONICS
+Y
-Y
-X
+X
+Z
-Z
FWD
ABBREVIATED COMPONENT MAINTENANCE MANUAL
TASK 25-62-11-990-802
2.Model Descriptions
SUBTASK 25-62-11-990-001
A.C406-2
(1)The C406-2 is a type AF (Automatic Fixed) ELT, which transmits on 121.5, 243.0, and 406
MHz.
(2)The ELT is enclosed within a multi-piece mounting frame consisting of a mounting tray,
protective top cover and mounting frame cap.
(3)When ordered as a system, an installation kit, cockpit remote switch, coax cables, audible
buzzer, and dual input antenna are provided.
SUBTASK 25-62-11-990-002
B.C406-2HM
C406-2 (453-5000), C406-2HM (453-5001)
(1)The C406-2HM ELT was developed for helicopter installations and features an additional 5-
axis G-Switch module, which allows the ELT to be activated in any of six axes. See "Figure 1.
ELT Orthogonal Axes".
(2)The C406-2HM ELT is identical to the C406-2 ELT in all other aspects.
Figure 1. ELT Orthogonal Axes
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
TASK 25-62-11-990-803
3.Approvals
SUBTASK 25-62-11-990-001
A.C406-2 and C406-2HM
(1)FAA TSO C126, Type AF
NOTE
:Details of TSO certification for the C406-2 Series ELT are available in the “C406-2
Series TSO Report” (572-0005, Issue 2).
(a)The conditions and tests required for TSO approval of this article are minimum
performance standards. It is the responsibility of those installing this article either on or
within a specific type or class of aircraft to determine that the aircraft installation
conditions are within TSO standards. TSO articles must have separate approval for
installation in an aircraft. The article may be installed only if performed under 14 CFR
Part 43 or the applicable airworthiness requirements.
(2)Transport Canada - Type Certificate Data Sheet AP-47 Issue 2
C406-2 (453-5000), C406-2HM (453-5001)
(3)Industry Canada - Certification Number 1215873110AF
(4)JTSO-2C126
(5)COSPAS-SARSAT - Certificate No. 112 or 170
SUBTASK 25-62-11-990-002
B.Battery
CAUTION
(1)The lithium battery pack used on the C406-2 Series ELT is certified under TSO C142.
SUBTASK 25-62-11-990-003
:LITHIUM BATTERY SAFETY CONCERNS INCLUDE THE POSSIBILITY OF FIRE, VENTING
VIOLENTLY, AND VENTING OF TOXIC GASES.
NOTE
:Details of TSO certification are available in the “452-0133 - 406 Lithium Battery Pack
TSO C142 Report” (572-0043).
(a)The conditions and tests required for TSO approval of this battery are minimum
performance standards. It is the responsibility of those desiring to install this battery in a
specific type or class of aircraft to determine that the aircraft installation conditions are
within the TSO standards. The battery may be installed only if further evaluation by
applicant documents an acceptable installation and is approved by the Administrator.
(2)The DO-160D environmental categories breakdown is detailed in Table 1, on page 19.
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
Table 1. Environmental Categories Breakdown
CATEGORYSECTIONDESCRIPTION
C14.0Temperature/Altitude
-4.5.4In-Flight Loss of Cooling
B5.0Temperature Variation
A6.0Humidity
2047.0/8.0Operational Shock and Crash Safety/Vibration
X9.0Explosion
R10.0Waterproofness
X11.0Fluids Susceptibility
X12.0Sand and Dust
X13.0Fungus
X14.0Salt Spray
X15.0Magnetic Effect
Z16.0Power Input
A17.0Voltage Spike
Z18.0Audio Frequency Susceptibility
Z19.0Induced Signal Susceptibility
20420.0Radio Frequency Susceptibility
B21.0Emission of RF Energy
X22.0Lightning
X23.0Lightning Direct Effects
X24.0Icing
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
TASK 25-62-11-990-804
4.Frequency Allocations
SUBTASK 25-62-11-990-001
A.Application
(1)This section addresses the 406.0-406.1 MHz transmitter window and the specific frequency
band allocations residing above 406.025 MHz, beginning with 406.028 MHz, which are
assigned or reserved within the 406.0-406.1 MHz distress frequency window.
SUBTASK 25-62-11-990-002
B.Discussion
(1)The 406 MHz transmitter frequency of the C406-2 Series ELT was originally 406.025 MHz. In
order to comply with COSPAS-SARSAT frequency allocation requirements, changes to the 406
MHz frequency may occur since the original release of this product.
(2)While the original C406-2 Series ELTs covered by this manual transmit on 406.025 MHz,
current C406-2 Series ELTs may not. The product identification label on each ELT specifies the
transmitting frequencies of the individual ELT. The 406 MHz component may be 406.025,
406.028, 406.037 MHz, etc. Allocation of frequencies, based on beacon population per
specified frequency band, is controlled by COSPAS-SARSAT.
C406-2 (453-5000), C406-2HM (453-5001)
(3)The frequency references throughout this manual for the 406 MHz component should be
considered the baseline and the specific frequency indicated on the ELT product label should
be substituted if it differs from 406.025 MHz.
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
TASK 25-62-11-990-805
5.List of Acronyms, Abbreviations, and Definitions
SUBTASK 25-62-11-990-001
Term
ACAdvisory Circular – A Federal Aviation Administration (USA) bulletin
AWGAmerican Wire Gauge – An electrical wire diameter standard. Look for
BNC CONNECTORA very common type of coax cable connector having a 50 imped-
CARCanadian Aviation Regulations – The rules and regulations governing
CFRCode of Federal Regulations – The general and permanent rules pub-
CONTAINERThe term “Container”, within the context of this document, refers to a
Definition
with special information. For the purposes of this document, the acronym AC does not refer to electrical alternating current.
this acronym in front of or following a wire size number.
ance and used for RF signal connections.
the manufacture, certification, operation, maintenance, and alteration
of aircraft in Canada.
lished in the Federal Register by the executive departments and
agencies of the Federal Government. Title 14, “Aeronautics and
Space” contains the FARs.
device designed to suppress RF signals, such that the broadcast of an
ELT placed in the container cannot reach the SAR satellite system.
COSPAS-SARSATThe international search and rescue consortium that governs the
international satellite-based search and rescue distress alert detection
and information distribution system. For a complete description go to
the official web site for the International COSPAS-SARSAT Program.
DERDesignated Engineering Representative – An individual qualified and
designated by the FAA to approve, or recommend approval, of technical data to the FAA.
DRIP LOOPExtra wire length used to form a U-shaped bend in a wire or cable.
Water or other fluids will flow down to the bottom of the loop and
drip off. Electrical connections are made at the top of the loop.
ELTEmergency Locator Transmitter – ELTs are installed on aircraft and
used to send emergency signals to the SAR satellite system. The
word “Beacon” is associated with these devices.
EMIElectromagnetic Interference – An undesirable disturbance that
affects an electrical circuit due to either electromagnetic conduction
or electromagnetic radiation emitted from an external source. Also
called radio frequency interference or RFI.
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
EUROCAEEuropean Organization for Civil Aviation Equipment – EUROCAE docu-
ments are widely referenced as a means of compliance to European
Technical Standard Orders (ETSOs) and other regulatory documents.
FAAFederal Aviation Administration – The United States government
agency for aircraft safety and regulation.
FARFederal Aviation Regulations – The rules and regulations governing
the manufacture, certification, operation, maintenance, repair, and
alteration of aircraft in the United States.
FORM 337FAA Form 337 is required anytime a major repair and/or major altera-
tion is performed on an aircraft. Refer to FAR, Part 43, Appendix A
and the definitions of Major Repair/Alteration contained in FAR, Part 1
for guidance.
FSDOFlight Standards District Office – FAA district offices responsible for
aircraft certification, operation, maintenance, and modification issues,
approvals and enforcement.
G-SWITCHA velocity switch that detects sudden de-acceleration and is used to
automatically activate an ELT. May also be referred to as a “crash
sensor”.
LEDLight Emitting Diode – Semiconductor device that emits light when
current is passed through it. Usually used as a status or warning indicator.
MILThe three-letter acronym that stands for “Military” and proceeds mili-
tary specifications and standards numbers (e.g., MIL-W-xxxx would
indicate a wire specification and MIL-STD-xxxx would indicate a standard).
P/NPart Number – Refers to a Wulfsberg Electronics part number, unless
otherwise noted. Part numbers are also indicated with parentheses
(e.g., XXX-XXXX).
PLUGThe term “Plug”, within the context of this document, refers to the
male half of an electrical connector.
RECEPTACLEThe term “Receptacle”, within the context of this document, refers to
the female half of an electrical connector.
RFRadio Frequency – The range of electromagnetic radiation that con-
stitutes the radio spectrum and corresponds to the frequency of alternating current electrical signals used to produce and detect radio
waves.
RTCARadio Technical Commission for Aeronautics – Organization that
RTVA rubbery silicon-based adhesive typically used to prevent vibration
makes recommendations for airworthiness. Refer to http://
www.rtca.org/aboutrtca.asp for more information.
problems and water intrusion.
Page 22 of 90
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COBHAM AVIONICS WULFSBERG ELECTRONICS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
SARSearch and Rescue
SCREEN ROOMThe term “Screen Room”, within the context of this document, refers
to a room designed to suppress RF signals, such that the broadcast of
an ELT placed in the screen room cannot reach the SAR satellite system.
SERVICE LOOPA length of wire or cable, at the connection point, of sufficient length
to allow a component to be withdrawn from its mounting position and
disconnected from its associated wiring.
TETHERA tether is a cord or similar device that anchors something movable
to a stationary point or anchors two items together, such that they
cannot become separated beyond the length of the tether.
TNC CONNECTORA threaded version of a BNC connector.
TPS CONNECTORA small, rugged, three-pin bayonet locking connector designed for
use when space and weight limitations are of primary concern.
TSOTechnical Standard Order – A TSO is a minimum performance stan-
dard issued by the FAA for specified materials, parts, processes, and
appliances used on civil aircraft.
UTCCoordinated Universal Time – A time standard based on International
Atomic Time. UTC is the time system used in aviation and is often
associated with Greenwich Mean Time (GMT) and/or “Zulu” time.
VHFVery High Frequency – The 30 MHz to 300 MHz radio frequency band.
VSWRVoltage Standing Wave Ratio – Electrical signals will “echo” back on a
wire if load impedance is not matched to the impedance of the wire.
VSWR is a measurement of the amount of voltage being “echoed,”
compared to the original signal.
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
TASK 25-62-11-990-806
6.References
SUBTASK 25-62-11-990-001
A.Regulatory Documents
(1)The following regulatory documents are referred to herein. When referring to such
documents, it is the manual user’s responsibility to ensure they are using the latest revision or
release of such documents. To that end, the revision designator of specific document numbers
has not been included, with the exception of the RTCA document listing, which reflects the
revision level of the documents at the time of TSO testing and certification.
(2)Except in the case of a printed manual, reference documents available on-line or source
locations are linked to applicable web sites.
(3)United States
•AC 43-9, “Maintenance Records”
C406-2 (453-5000), C406-2HM (453-5001)
•AC 43-210, “Standardized Procedures for Requesting Field Approval of Data, Major
Alterations, and Repairs”
•AC 43.9-1, “Instructions for Completion of FAA Form 337”
•AC 43-13-1, “Acceptable Methods, Techniques, and Practices – Aircraft Inspection and
Repair”
•AC 43.13-2, “Acceptable Methods, Techniques, and Practices - Aircraft Alterations”
•FAR, Part 43, “Maintenance, Preventive Maintenance, Rebuilding, and Alteration”
•FAR, Part 91, “General Operating and Flight Rules”
(4)Canada
•CAR, Part V, “Airworthiness”
•CAR, Part VI, “General Operating and Flight Rules”
(5)COSPAS-SARSAT
•C/S G.005, “Cospas-Sarsat Guidelines on 406 MHz Beacon Coding, Registration and
Type Approval”
•C/S S.007, “Handbook of Beacon Regulations”
(6)RTCA – The following documents are available for purchase at RTCA’s web site www.rtca.org,
or by mail:
•DO-160D, “Environmental Conditions and Test Procedures for Airborne Equipment”
•DO-178B, “Software Considerations in Airborne Systems and Equipment Certification”
•DO-182, “Emergency Locator Transmitter (ELT) Equipment Installation and
Performance”
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
•DO-183, “Minimal Operational Performance Standards for Emergency Locator
Transmitters - Automatic Fixed-ELT (AF), Automatic Portable-ELT (AP), Automatic
Deployable-ELT (AD), Survival-ELT (S) Operating on 121.5 and 243.0 MHz”
(1)The ELT automatically activates during a crash and transmits the standard sweep tone on
121.5 and 243.0 MHz. Approximately every 50 seconds, for up to 520 milliseconds (long
message protocol), the 406 MHz transmitter turns on. During that time, an encoded digital
message is sent to the COSPAS-SARSAT Search and Rescue (SAR) satellite system.
(2) The information contained in the message includes:
(a)Serial number assigned to the ELT by the beacon manufacturer or the national beacon
registration authority, or
C406-2 (453-5000), C406-2HM (453-5001)
DESCRIPTION AND OPERATION
(b)Aircraft identification or registration number, and
(c)Country of registration and country code; plus
(d)Position coordinates, when coupled with an ELT/NAV Interface (453-6500). Refer to the
ELT/NAV Interface Abbreviated Component Maintenance Manual (570-4602) for a
detailed discussion of the interaction between the ELT, ELT/NAV Interface, and aircraft
navigation system.
(3)The 406 MHz transmitter will operate for 24 hours and then shuts down automatically. The
121.5/243.0 transmitter will continue to operate until the batteries are exhausted, which is at
least 50 hours.
(4)The 406 MHz transmitter produces a much more accurate position, typically 3 kilometers as
compared with 15 to 20 kilometers for 121.5/243.0 MHz transmitters. When coupled to the
aircraft navigation system via the ELT/NAV Interface, the accuracy improves to approximately
100 meters.
(5)The ELT transmits a digital message that allows search and rescue authorities to contact the
owner/operator of the aircraft through information contained in a database. Information
contained in the database includes:
(a)Type of aircraft and aircraft registration number,
(b)Owner address and telephone number, and
(c)Alternate emergency contact.
(6)After the ELT is activated and the 406 MHz signal is detected by the SAR satellite system and
a position is calculated, the 121.5/243.0 MHz transmissions are used to home in on the crash
site.
NOTE
:Effective February 1, 2009, COSPAS-SARSAT has terminated satellite processing of
distress signals from 121.5 and 243.0 MHz beacons.
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