DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
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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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
RECORD OF REVISIONS
REVISIONCHANGEDATEREVISIONCHANGEDATE
-RELEASEJun 30/2005
ADCN 2670Nov 17/2005
BDCN 2777May 01/2006
CDCN 2847Aug 21/2006
DDCN 3007May 21/2007
EDCN 3076Sep 27/2007
FDCN 3182Mar 03/2008
GDCN 3227May 19/2008
GDCN 3413Mar 30/2009
HDCN 3571Jan 12/2010
JDCA W9414Apr 06/2010
KECO 14756Jul 26/2011
LECO 14850Mar 09/2012
MECO 15380May 3/2013
NECO 15420Jun 25/2013
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
SERVICE BULLETIN LIST
SERVICE
BULLETIN NO
ISSUE
DATE
SUBJECT
MANUAL
REV NO
MANUAL
REV DATE
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ME406 (453-6603), ME406HM (453-6604)
LIST OF EFFECTIVE PAGES
SUBJECTPAGEDATESUBJECTPAGEDATE
Title Page1May 3/13Description and Operation (cont.)30May 3/13
Notices2May 3/13Test and Fault Isolation31May 3/13
Record of Revisions3May 3/1332May 3/13
Service Bulletin List4May 3/1333May 3/13
List of Effective Pages5May 3/1334Jun 25/13
6May 3/1335May 3/13
Table of Contents7May 3/1336May 3/13
8May 3/1337May 3/13
9May 3/1338May 3/13
10May 3/1339May 3/13
List of Figures11May 3/1340May 3/13
Introduction12May 3/1341May 3/13
13May 3/1342May 3/13
14Jun 25/1343May 3/13
15May 3/1344May 3/13
16May 3/13Removal45May 3/13
17May 3/1346May 3/13
18May 3/1347May 3/13
19May 3/13Installation48May 3/13
20May 3/1349May 3/13
21May 3/1350May 3/13
Description and Operation22May 3/1351May 3/13
23May 3/1352May 3/13
24May 3/1353May 3/13
25May 3/1354May 3/13
26May 3/1355May 3/13
27May 3/1356May 3/13
28May 3/1357May 3/13
29May 3/1358May 3/13
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ME406 (453-6603), ME406HM (453-6604)
SUBJECTPAGEDATESUBJECTPAGEDATE
Installation59May 3/1372May 3/13
(cont.)60May 3/1373May 3/13
61May 3/1374May 3/13
62May 3/1375May 3/13
63May 3/13Appendix A76May 3/13
64May 3/1377May 3/13
65May 3/13Illustrated Parts List78May 3/13
66May 3/1379May 3/13
67May 3/1380May 3/13
68May 3/1381May 3/13
69May 3/1382May 3/13
70May 3/1383May 3/13
71May 3/1384May 3/13
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
TASK 25-62-30-990-801
1.Manual Usage
SUBTASK 25-62-30-990-001
A.General
(1)This manual describes the operation, installation, and maintenance of the Model ME406 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 products web site at www.acrartex.com
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 76.
ME406 (453-6603), ME406HM (453-6604)
INTRODUCTION
for the
(3)Web links provided in this manual were accurate at time of printing, but may be subject to
change.
(4)ACR 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 25-62-30-990-002
B.Application
(1)This manual constitutes supporting data/documentation for the ME406 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 ME406 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 ME406 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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ARTEX PRODUCTS / ACR ELECTRONICS, INC
+Z
-Z
+X
-X
-Y
+Y
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
(4)ME406 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 ME406 Series ELT. Other options, such as a
different remote switch configuration or a navigation interface, should be installed and
maintained in accordance with the written instructions specific to the accessory.
NOTE
:Contact ACR Electronics, Inc., for optional accessories approved for use with a
ME406 Series ELT.
(6)To ensure proper operation, only parts listed in the Illustrated Parts List of this manual or
those recommended by ACR Electronics, Inc., may be used as replacement parts for the
ME406 Series ELT.
TASK 25-62-30-990-802
2.Model Descriptions
SUBTASK 25-62-30-990-001
ME406 (453-6603), ME406HM (453-6604)
A.ME406
(1)The ME406 is a type AF (Automatic Fixed) beacon, which transmits on 121.5 and 406 MHz.
(2)The ME406 ELT is enclosed in an impact resistant plastic casing and mounts on a tray made of
similar material.
(3)When ordered as a system, an installation kit, cockpit remote switch, coax cables, audible
buzzer, and fixed antenna are provided.
SUBTASK 25-62-30-990-002
B.ME406HM
(1)The ME406HM ELT is designed for helicopter installations and features a 5-axis G-Switch
module in addition to the primary G-switch, which is oriented to line-of-flight. This design
allows the ELT to be activated in all six axes. See Figure 1 ELT Orthogonal Axes.
(2)The ME406HM is identical to the ME406 in all other aspects.
Figure 1 ELT Orthogonal Axes
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TASK 25-62-30-990-803
3.Approvals
SUBTASK 25-62-30-990-001
A.ME406 and ME406HM
(1)FAA TSO C126, Type AF
(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 - Approval Letter File Reference 5012-E3-4 (3708020)
(3)Industry Canada - Certification Number 1215B-ME406AF
ME406 (453-6603), ME406HM (453-6604)
(4)ETSO 2C126 - EASA.IM.21O.416 (ME406) and EASA.IM.21O.608 (ME406HM)
(5)COSPAS-SARSAT - Certificate No. 152, 188, 197 and 242
SUBTASK 25-62-30-990-002
B.Battery
CAUTION
(1)The lithium battery pack used on the ME406 Series ELT is certified under TSO C126.
SUBTASK 25-62-30-990-003
C.RTCA DO-160D Compliance
(1)DO-160D Environmental Categories:
(2)The DO-160D environmental categories breakdown is detailed in Table 1 on page 14.
:LITHIUM BATTERY SAFETY CONCERNS INCLUDE THE POSSIBILITY OF FIRE, VENTING
VIOLENTLY, AND VENTING OF TOXIC GASES.
(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.
D1XBC[204][204]XRXXFXXZAZA[204]H[XXXX]XXA
Table 1 Environmental Categories Breakdown
CATEGORYSECTIONDESCRIPTION
D14.0Temperature/Altitude
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ME406 (453-6603), ME406HM (453-6604)
CATEGORYSECTIONDESCRIPTION
X4.5.4In-Flight Loss of Cooling
B5.0Temperature Variation
C6.0Humidity
2047.0/8.0Operational Shock and Crash Safety/Vibration
X9.0Explosion
R10.0Waterproofness
X11.0Fluids Susceptibility
X12.0Sand and Dust
F13.0Fungus
X14.0Salt Spray
X15.0Magnetic Effect
Z16.0Power Input
A17.0Voltage Spike
Z18.0Audio Frequency Susceptibility
A19.0Induced Signal Susceptibility
20420.0Radio Frequency Susceptibility
H21.0Emission of RF Energy
XXXX22.0Lightning
X23.0Lightning Direct Effects
X24.0Icing
A25.0ESD
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
TASK 25-62-30-990-804
4.Frequency Allocations
SUBTASK 25-62-30-990-001
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 25-62-30-990-002
B.Discussion
(1)The 406 MHz transmitter frequency of the ME406 Series ELT was originally 406.028 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 ME406 Series ELTs covered by this manual transmit on 406.028 MHz,
current ME406 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 406.028,
406.037 MHz, etc. Allocation of frequencies, based on beacon population per specified
frequency band, is controlled by COSPAS-SARSAT.
ME406 (453-6603), ME406HM (453-6604)
(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 406.028 MHz.
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
TASK 25-62-30-990-805
5.List of Acronyms, Abbreviations, and Definitions
SUBTASK 25-62-30-990-001
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 W 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.
D-SUB CONNECTORD-shaped, subminiature connectors – common type of connector for
small signals and electrical currents.
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
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
or electromagnetic radiation emitted from an external source. Also
called radio frequency interference or RFI.
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 alter-
ation 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 an ACR part number, unless otherwise
noted. Part numbers are also indicated with parentheses (e.g., XXXXXXX).
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.
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
RTCARadio Technical Commission for Aeronautics – Organization that
makes recommendations for airworthiness. Refer to
www.rtca.org/aboutrtca.asp
RTVA rubbery silicon-based adhesive typically used to prevent vibration
problems and water intrusion.
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.
for more information.
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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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
TASK 25-62-30-990-806
6.References
SUBTASK 25-62-30-990-001
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
(a)AC 43-9, “Maintenance Records”
ME406 (453-6603), ME406HM (453-6604)
(b)AC 43-210, “Standardized Procedures for Requesting Field Approval of Data, Major
Alterations, and Repairs”
(c)AC 43.9-1, “Instructions for Completion of FAA Form 337”
(d)AC 43-13-1, “Acceptable Methods, Techniques, and Practices – Aircraft Inspection and
Repair”
(e)AC 43.13-2, “Acceptable Methods, Techniques, and Practices - Aircraft Alterations”
(f)FAR, Part 43, “Maintenance, Preventive Maintenance, Rebuilding, and Alteration”
(g)FAR, Part 91, “General Operating and Flight Rules”
(4)Canada
(a)CAR, Part V, “Airworthiness”
(b)CAR, Part VI, “General Operating and Flight Rules”
(5)COSPAS-SARSAT
(a)C/S G.005, “Cospas-Sarsat Guidelines on 406 MHz Beacon Coding, Registration and
Type Approval”
(b)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:
,
(a)DO-160D, “Environmental Conditions and Test Procedures for Airborne Equipment”
(b)DO-178B, “Software Considerations in Airborne Systems and Equipment Certification”
(c)DO-182, “Emergency Locator Transmitter (ELT) Equipment Installation and
Performance”
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
(d)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”
(e)DO-204, “Minimal Operational Performance Standards for 406 MHz Emergency Locator
Transmitters (ELT)”
SUBTASK 25-62-30-990-002
B.Other Documents
(1)The following documents are available on-line at the Artex products web site at
www.acrartex.com
(a)570-1000, “ELT Test Set (ETS) Operation Manual”
ME406 (453-6603), ME406HM (453-6604)
, or from ACR Electronics upon request.
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TASK 25-62-30-870-801
1.Description
SUBTASK 25-62-30-870-001
A.Functional Overview
(1)The ELT automatically activates during a crash and transmits the standard sweep tone on
121.5 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
ME406 (453-6603), ME406HM (453-6604)
DESCRIPTION AND OPERATION
(b)Aircraft identification or registration number, and
(c)Country of registration and country code; plus
(d)Position coordinates, when coupled with a navigation interface device, which receives
position data from the aircraft navigation system and transmits it to the ELT.
(3)The 406 MHz transmitter will operate for 24 hours and then shuts down automatically. The
121.5 MHz 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 MHz transmitters. When coupled to the aircraft
navigation system via a navigation 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 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 MHz beacons.
(7)Aircraft communications transceivers are not capable of receiving 406 MHz transmissions;
therefore, the only methods of monitoring the ELT are:
(a)The blinking cockpit remote switch LED,
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DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
(b)The buzzer, or
(c)121.5 MHz transmissions, which can be monitored using the aircraft communications
transceiver or an AM radio tuned to 121.5 MHz.
SUBTASK 25-62-30-870-002
B.Components
(1)The ME406 Series ELT main assembly is housed in a high impact, fire resistant, polycarbonate
plastic case and mounted in a tray made of similar material. See Figure 2 ME406 Series ELT
and Mounting Tray Assembly.
NOTE
:The ELT main assembly and its mounting frame assembly are capable of
withstanding extremely harsh environments and have been subjected to the rigorous
environmental testing required by COSPAS-SARSAT for certification.
CONTROL
SWITCH
ME406 (453-6603), ME406HM (453-6604)
ANTENNA BNC
STATUS
CONNECTOR
LED
A
REMOTE SWITCH
D-SUB RECEPTACLE
ELT MAIN
ASSEMBLY
MOUNTING
TRAY ASSY
OPTIONS
Figure 2 ME406 Series ELT and Mounting Tray Assembly
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ARTEX
ON
ARM
Press ON
Wait 1 Second
Press ARM
EMERGENCY USE ONLY
Test/Reset
ELT
LED
SWITCH
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
(2)The cockpit-mounted remote switch assembly is comprised of an ELT status LED and control
switch, and allows an operator to manually turn the ELT on (i.e., activate) for testing and
reset (i.e., deactivate) the ELT. See Figure 3 Remote Switch Front View.
NOTE
:The ELT CANNOT be disarmed or disabled from the cockpit. Cockpit operation is
limited to deactivating or manually activating the ELT.
Figure 3 Remote Switch Front View
(3)The buzzer (i.e., horn) provides an audible alert when the ELT is active. See Figure 4 Buzzer.
Figure 4 Buzzer
(4)The battery pack for the ME406 Series ELT consists of two “D” size lithium manganese dioxide
cells connected in series. To prevent the cells from being charged, diodes are connected
across each cell and fuses are connected to the output. See Figure 5 Battery Pack Assembly.
(5)Two antennas are approved for use with the ME406 Series ELT. Selection of the proper
Figure 5 Battery Pack Assembly
antenna is dependent upon end use, aircraft configuration and speed, and other factors. See
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110-773
110-338
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
ME406 (453-6603), ME406HM (453-6604)
Figure 6 Antennas.
Figure 6 Antennas
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ELT
“INACTIVE”
ELT “ACTIVE”
BUZZER “ON”
LED “ON”
ELT
SWITCH
“ON”
REMOTE
SWITCH
“ON”
G-SWITCH
“ON”
ELT OR
REMOTE SW
“RESET”
YES
YES
NO
NO
NO
YES
NO
YES
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
TASK 25-62-30-870-802
2.Operation
SUBTASK 25-62-30-870-001
A.Operational Overview
(1)See Figure 7 ELT Operational Flow Diagram.
ME406 (453-6603), ME406HM (453-6604)
Figure 7 ELT Operational Flow Diagram
(2)A primary feature of the ME406 Series ELT is its simplicity of operation. As long as the ELT is
connected to the remote switch harness ELT connector, such that pins 5 and 12 are jumpered
(G-switch loop), it will activate in the event of a crash.
NOTE
:Neither the cockpit remote switch or the ELT local switch can be positioned in such a
manner as to prevent automatic activation when the ELT is connected properly.
(3)ELT operation is designed to prevent human error and misuse in regards to automatic
activation. The ELT cannot be activated by dropping, rough handling or during shipping.
(4)When the ELT is activated, the presence of the emergency sweep tone and the flashing
cockpit remote switch panel LED indicates an active, normal functioning ELT. The cockpit
panel LED must immediately begin to flash continuously upon ELT activation.
(5)The ELT is considered to be either “ACTIVE” or “INACTIVE”. When “INACTIVE”, the ELT is in a
state of rest and performs no functions. Taking the ELT from the “INACTIVE” state to the
“ACTIVE” state requires a positive switch transition from either the cockpit remote switch, ELT
local switch, or G-switch.
Page 26 of 84
25-62-30
Jun 25/13
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