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General| Brand | Kannad |
|---|---|
| Model | S1822502-02 |
| Category | Transmitter |
| Language | English |
Details on the launch, purpose, and components of the COSPAS-SARSAT system.
Explains the global coverage and benefits of the COSPAS-SARSAT system for aeronautical emergencies.
Details the severe mechanical and environmental tests ELTs undergo for certification.
Discusses the role and optimization of G-Switch sensors in ELTs for crash detection accuracy.
Lists and describes the main components of the KANNAD 406 ELT system.
Details the Transmitter, Bracket, Remote Control Panel, and Outside Antenna components.
Covers general design aspects and mechanical construction of the ELT unit.
Explains how the transmitter is activated and transmits on multiple frequencies.
Details the 3-position switch, visual indicator, connectors, and buzzer functions.
Describes the Off, Self-Test, Armed, and On modes of operation.
Details the conditions and procedures for the 'OFF' mode of the ELT.
Explains the self-test mode, its purpose, and how to interpret results.
Describes the 'ARM' mode for standby activation and its mandatory use during flight.
Explains the 'ON' mode for transmission, including activation triggers and signal behavior.
Details the battery power, transmission autonomy, and battery replacement schedule.
Covers power supply, electrical interface, and connector pin-outs.
Details the connectors and wiring for the Remote Control Panel and antenna.
Lists detailed technical specifications including frequencies, output power, and environmental conditions.
Explains standby and manual activation methods for the ELT.
Details the 'ARM' mode for automatic activation via crash sensor or remote panel.
Describes how to manually activate the ELT using the ON switch.
Explains how to stop the ELT in case of unintentional activation.
Procedure for resetting the ELT by switching it to OFF then ARM.
Procedure for resetting the ELT using the remote control panel.
References the self-test procedure located on page 301.
Outlines regulatory recommendations for ELT installation and mounting.
Details the mandatory ELT registration and programming procedures.
Explains the pin-programming capability using a Programming Dongle.
Step-by-step guide for mounting the ELT bracket and transmitter.
Guide for performing initial power-up tests after installation.
Specific mounting instructions for the KANNAD 406 AF on fixed wings and helicopters.
Specific mounting instructions for the KANNAD 406 AF-H on helicopters.
Specific mounting instructions for the KANNAD 406 (6D) on aircraft.
Step-by-step guide for safely removing the ELT from the aircraft.
Details the periodicity and procedure for performing ELT self-tests.
Recommends monthly self-tests and cautions against excessive testing.
Step-by-step guide on how to perform the ELT self-test and interpret results.
Describes tests for installation without and with a programming dongle.
Steps for testing ELT operation after installation without a programming dongle.
Steps for testing ELT operation with a programming dongle and maintenance dongle.
Details how to check the operation of the RCP LED and buzzer.
Describes tests for ELT-Antenna link, 406 MHz, and 121.5 MHz transmission.
Explains how to check the ELT-Antenna link using VSWR measurement.
Procedure for testing 406 MHz transmission with a COSPAS-SARSAT decoder.
Procedure for testing 121.5 MHz transmission using a VHF receiver.
Introduction to troubleshooting using the ELT's front panel visual indicator.
Explains fault indications from the visual indicator during self-test.
Details the meaning of flash codes (3+1, 3+2, 3+3, 3+4) for self-test failures.
Covers faults related to the buzzer operation.
Troubleshooting for buzzer not operating or operating permanently.
Provides dimensional drawings and measurements of the ELT and bracket.
Shows the drilling pattern and hole locations for mounting the ELT bracket.
Illustrates the electrical connections between the ELT, remote panel, and antenna.
Outlines periodic inspections and battery replacement requirements.
Details parameters to check during periodic inspections as required by authorities.
Covers mandatory 6-year checks, including battery replacement and tightness.
Mandatory conditions and recommendations for replacing the ELT battery.
