EMERGENCY BEACON CORPORATION EBC-406HM Manuale di istruzioni e manutenzione - Pagina 4

Sfoglia online o scarica il pdf Manuale di istruzioni e manutenzione per Trasmettitore EMERGENCY BEACON CORPORATION EBC-406HM. EMERGENCY BEACON CORPORATION EBC-406HM 11. Emergency locator transmitter

SECTION 1

GENERAL DESCRIPTION

The EBC-406HM is an Emergency Locator Transmitter (ELT)
designed for military helicopter installation. It meets the requirements
of TSO-C126 in the Automatic Portable (AP) category (see Figures 1
& 2). It is designed for mounting in the cabin of the aircraft, within reach
of the pilot or co-pilot. As with all EBC ELTs, the increased survivability
needs of cabin mounting have been met. The electronics and the
activation system are completely encapsulated, and extra protection
has been provided for the crystal. Our encapsulation method provides
added protection against shock and moisture. The ELT transmits on
406.028 MHz, the civil 121.5 MHz, and the military 243.0 MHz
emergency frequencies.
A unique characteristic of helicopter performance is that in the event
of a loss of power, a helicopter may not necessarily go down nose first
and may not have any forward motion. This may render a single axis
G-switch ineffective. The EBC-406HM has two special G-switches that
can sense deceleration forces from all directions, making it uniquely
suited for helicopter use. These 360° spherical switches are identical
to those used and proven in our original helicopter ELTs (our EBC-
302HM, EBC-302VRHMJ-121.5, EBC-302VRHMJ-243.0, EBC-
302VHMJ, and EBC-502HM models). They will not trigger during a
hard landing.
The EBC-406HM system has an LED (on the ELT) and buzzer (on the
mounting bracket/tray) to indicate ELT activation, and self-test results.
The LED and toggle switch are recessed to provide added protection
against damage and inadvertent activation.
The bottom of the ELT houses a recessed D-Sub connector that mates
with the mounting bracket/tray connector. The mounting bracket/tray
connector is wired to a buzzer, and also wired with a G-switch loop;
this loop-back enables the G-switch when properly mated to the ELT
connector.
To prevent inadvertent activation, the ELT G-switches are disabled
when the ELT is removed from its mount.
No external power connections are required. All indicators and controls
are powered from the ELT's battery pack. Installation near the pilot
eliminates the need for a wire harness and Remote Control Monitor.

SECTION 2

REGISTERING YOUR ELT

It is required that every 406 ELT be registered by the aircraft owner
after installation, re-registered every two years, and re-registered if
there are any changes to information provided to JSETS in a previous
registration, such as telephone numbers, aircraft registration number,
change of owner, ...etc.
Every 406 ELT is programmed at the factory with a unique
identification code used by the Rescue Coordination Center to
determine if an emergency has occurred. This identifier is called the
15-Hex ID. It is located on the front label of the ELT.
This unique identifier is stored in a database maintained by
DOD/JSETS. It can be accessed to contact the owner in the event of
ELT activation. Registration is free, and can even be done via the
Internet. See the Airworthiness Release for further instructions on
registration.
Make sure that the 15-Hex ID on the front label of the ELT is properly
entered on the form. Also, enter all required information. Once you
receive your registration confirmation, review it carefully. Failure to
register or re-register as required every two years or to notify JSETS
of any changes to the status of your 406 MHz beacon could result in
penalties or unnecessary delays in search and rescue operations.

SECTION 3

TOGGLE SWITCH FUNCTIONS

The EBC-406HM must be installed in the cabin of the aircraft, within
reach of the pilot or co-pilot, for easy access in an emergency.
ON position:
This position (closest to the antenna connector) manually activates the
ELT. The ELT will begin radiating a distress signal on 121.500 MHz,
243.000 MHz, and within 50 seconds, will radiate an emergency coded
signal on 406.028 MHz.
ARM position:
This position (center position) is the normal operating position for the
ELT. When properly installed in its mount, the ELT is armed and ready
to activate if an accident is sensed. When removed from its mount, the
G-switch is disabled, and any mishandling will not result in activation;
the ELT can still be activated by setting the toggle switch to the "ON"
position.
TEST-RESET position:
This position (closest to the LED) is used to self-test, and to deactivate
the ELT.
To deactivate the ELT, momentarily hold the toggle switch in this
position (closest to LED), for about one second and quickly release.
The ELT will perform a self-test, and then deactivate. Refer to
Sections 6 and 7 for self-test instructions and results.
To self-test the ELT, momentarily move the handle from the center
position to the "TEST-RESET" position; hold for about one second and
quickly release. The ELT will perform a self-test and then deactivate.
Refer to Sections 6 and 7 for self-test instructions and results.
It is recommended that the homer signal be monitored on a radio
tuned to 121.500 MHz.
DISABLING THE AUTOMATIC ACTIVATION FEATURE
The ELT G-switch is disabled when the ELT is removed from its mount,
and enabled ONLY when the ELT is installed and properly mated to
its mounting bracket/tray connector. The mounting bracket/tray
connector has a loop-back installed at the factory. The loop-back is
checked by the self-test.
A "2 code" indicates a disabled G-switch.
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