Do you have a question about the EMERGENCY BEACON CORPORATION EBC-406HM and is the answer not in the manual?
Manually activates the ELT, transmitting distress signals on multiple frequencies.
Normal operating position; ELT is armed to activate if an accident is sensed.
Used to perform self-tests and deactivate the ELT; requires a quick release.
Details the procedure for gently installing the ELT into the BB-12M mount and securing the latch.
Explains how to slide the connector forward and insert the ELT into the BB-15M tray, then secure the latch.
Covers in-bracket and out-of-bracket self-tests to verify ELT functionality.
Verifies 121.5 MHz power, signal output, LED/buzzer indicators, and loop-back function.
Details how to verify G-switch functionality through manual activation tests.
Procedures for removing the ELT from both BB-12M and BB-15M mounting systems.
Advise to place the ELT on high ground with antenna vertical for best operation.
Covers inspection of antenna, connectors, battery pack, and performing full functional tests.
Step-by-step guide on how to safely replace the ELT battery, including precautions.
Instructions on contacting the factory for repair, shipping the ELT (without battery), and warranty details.
The EBC-406HM is an Emergency Locator Transmitter (ELT) specifically designed for military helicopter installations. It meets the requirements of TSO-C126 in the Automatic Portable (AP) category. This ELT is intended for cabin mounting within the aircraft, easily accessible to the pilot or co-pilot. Its design emphasizes increased survivability through cabin mounting. The device's electronics and activation system are fully encapsulated, with additional protection for the crystal, enhancing resistance to shock and moisture. The EBC-406HM transmits on three emergency frequencies: 406.028 MHz, the civil 121.5 MHz, and the military 243.0 MHz.
A key feature for helicopter use is its unique G-switch system. Unlike single-axis G-switches that might be ineffective in certain helicopter crash scenarios (where a loss of power doesn't always result in a nose-first descent or forward motion), the EBC-406HM incorporates two special G-switches. These switches are designed to sense deceleration forces from all directions, providing 360° spherical detection. This system is identical to those used in previous EBC helicopter ELT models and is engineered not to trigger during a hard landing, ensuring activation only in true emergency situations.
The EBC-406HM system includes an LED on the ELT unit and a buzzer on the mounting bracket/tray. These indicators provide visual and auditory feedback for ELT activation and self-test results. Both the LED and the toggle switch are recessed to protect against damage and inadvertent activation. A recessed D-Sub connector on the ELT's bottom mates with the mounting bracket/tray connector. This bracket/tray connector is wired to the buzzer and includes a G-switch loop-back, which enables the G-switch when the ELT is properly mated to its connector. To prevent accidental activation, the ELT's G-switches are disabled when the unit is removed from its mount. The ELT operates independently, requiring no external power connections, as all indicators and controls are powered by its internal battery pack. Installing the ELT near the pilot eliminates the need for a separate wire harness and Remote Control Monitor.
The EBC-406HM must be installed in the aircraft cabin, within reach of the pilot or co-pilot, for quick access during an emergency. The toggle switch has three positions:
The automatic activation feature is disabled when the ELT is removed from its mount and is only enabled when the ELT is installed and properly mated to its mounting bracket/tray connector. The mounting bracket/tray connector has a factory-installed loop-back, which is checked during the self-test. A "2 code" indicates a disabled G-switch.
Registration of every 406 ELT by the aircraft owner is mandatory after installation, with re-registration required every two years and whenever there are changes to the information provided to JSETS (e.g., telephone numbers, aircraft registration number, change of owner). Each 406 ELT is factory-programmed with a unique 15-Hex ID, located on the front label, which is used by the Rescue Coordination Center for identification during emergencies. This identifier is stored in a DOD/JSETS database to facilitate contact with the owner. Registration is free and can be done online. It is crucial to ensure the 15-Hex ID and all other required information are correctly entered on the registration form. Failure to register or re-register can lead to penalties or delays in search and rescue operations.
Periodic inspections are based on FAA, AC 43.13-1B CHG 1. The FCC mandates that transmitter tests be performed only during the first 5 minutes of each hour and last no longer than 3 audio sweeps of the ELT signal. This test must be performed at least once a year. Inspection steps include:
Battery replacement is required by FAR 91.207(c) when the replacement date marked on the ELT or battery is reached, or after one cumulative hour of transmitter use. The battery replace label is on the ELT's exterior and on the battery itself. The battery pack must be replaced every 5 years or after one hour of cumulative use. Batteries should not be stored outside the ambient temperature range of -40°C to 80°C. Only battery P/N GS-46 is approved; using other batteries will void TSO-C126 compliance.
The battery installation procedure involves:
The replacement battery pack part number is GS-46. The battery pack contains three lithium manganese dioxide cells. Users are cautioned not to disassemble, short circuit, or dispose of the battery pack in or near fire or flame, as lithium is flammable. Lithium battery safety concerns include the possibility of fire, violent venting, and toxic gases.
For repairs, users should contact the factory for advice if experiencing problems. If repairs are necessary, the battery should be removed, and the ELT (without the battery) should be sent to the factory. Emergency Beacon Corporation is the only authorized repair facility. A note describing the problem should be included, and EBC will evaluate the unit and provide a repair estimate. A nominal fee applies for inspection unless the ELT is under warranty. Shipping costs to and from the factory are borne by the customer.
| Frequency | 406 MHz |
|---|---|
| Dimensions | 2.2" x 4.4" |
| Battery Life | >24 hours @ -4°F (-20°C) |
| Operating Temperature | -20°C to +55°C |
| Power Output | 5 W |
| Type | Emergency Beacon |
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