Kannad 406 ap
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The Kannad 406 AP is an automatic portable emergency locator transmitter (ELT) that operates on three frequencies and offers advantages over conventional two-frequency ELTs including global coverage through multiple satellites, precise location pinpointing, and identification of aircraft in distress. It can be installed near the tail of an aircraft and activated automatically in a crash or manually. When removed from its bracket, it functions as a portable survival beacon. Programming is quick and maintenance is limited to monthly self-tests.
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Kannad 406 ap
- 1. Kannad 406 AP Automatic portable COSPAS-SARSAT ELT three frequency transmitter Advantages Description This new generation ELT offers all the latest improvements of the COSPAS-SARSAT system with the 406 MHz frequency at a price slightly over that of conventional two frequency ELTs: Specialist in pinpointing distresses by satellite and number one in 406 MHz maritime Emergency Position Indicating Radio Beacons (EPIRBs), KANNAD proposes the Kannad 406 AP, Automatic Portable Emergency Locator Transmitter (ELT). - Global coverage thanks to COSPAS-SARSAT multiple satellite constellation - Precise pinpointing (<1NM) due to the unparalleled frequency accuracy of the 406 transmitter The Kannad 406 AP is designed to be installed near the tail and to be connected to an outside antenna. A sophisticated 束 shock sensor 損 will activate the ELT automatically in the event of a crash. When removed from its bracket and connected to the auxiliary antenna, the Kannad 406 AP becomes an autonomous survival beacon operating on 3 frequencies (121,5/243,0/406MHz). - Identification of the aircraft in distress the ELT transmits a unique aircraft identification number Screw the antenna AN T ARM OFF ON RC - Efficient process of false alarms to avoid costly search and rescue operations AN T ARM OFF ON RC Switch on ON position AN T AR M OF F ON RC Distributor & Repair Station www.gelbyson.com - E-mail: info@gelbyson.com www.kannad.com
- 2. Kannad 406 AP A buzzer and a led integrated to the ELT warns the pilot should an activation occur. A navigation interface (ARINC429 or RS serial) can be added (on option) to download the position of the aircraft in the ELT. In this case COSPAS-SARSAT organisation will receive the position in addition to the identification of the aircraft instantly. Maintenance is limited to a monthly 束 self test 損 and the lamp flashing sequence indicates the test result. Battery replacement is only necessary every 6 years thanks to LiMnO2 technology. This represents a considerable improvement over standard generation ELTs with battery replacement necessary every year or every two years. The Kannad 406 AP is qualified in EUROPE with JTSO-2C91a & JTSO-C126 in compliance with EUROCAE ED62 standard and by FAA with TSO-C91a and TSO-C126. P/N P/N: S1820502-02 ELT KANNAD 406 AP P/N: S1820511-01 mounting bracket - 1 strap OPTIONS: SMART CONNECTORS P/N: S1820514-01 PROGRAMMING DONGLE P/N: S1820514-02 DEPROGRAMMING MAINTENANCE DONGLE OPTIONS: NAVIGATION INTERFACE P/N: S1825501-02 NAV. INTERFACE (ARINC 429) P/N: S1825501-01 NAV. INTERFACE (SERIAL RS) OPTIONS: REMOTE CONTROL PANELS P/N: S1820513-11 REMOTE CONTROL PANEL RC200 (33 x 50mm) P/N: S1820513-05 REMOTE CONTROL PANEL RC400 (148 x 38mm) OPTIONS: ANTENNAS P/N: 0124220 ANTENNA FOR LOW SPEED AIRCRAFT ANT 300 P/N: 0124251 ANTENNA FOR HIGH SPEED AIRCRAFT ANT 650 CONTACT US FOR REMOTE CONTROL AND ANTENNA SELECTION Distributor & Repair Station www.gelbyson.com - E-mail: info@gelbyson.com POWER SUPPLY Solid Cathode Lithium battery pack (LiMnO2) Battery replacement every 6 years PROGRAMMING . Aircraft nationality and registration marking . Aircraft operator designator and ELT serial number up to 4096 . Aircraft ICAO 24 bit address . Serial number . Pin programming connector on option ACTIVATION Automatically by an integrated shock sensor (G-SWITCH) Manually Remotely (remote control panel in the cockpit) SELF TEST 406 MHz RF power Battery voltage Frequency Programming TEMPERATURE RANGE Operating: -20属C to +55属C Storage: -55属C to +85属C KANNAD reserves the right to modify any of above specifications without notice. Not contractual photos. A remote control panel (on option) located in the cockpit allows manual activation and the self test of various operating parameters. TRANSMISSION 406.025 MHz 5W (37 賊2dBm) Modulation 16K0G1D (bi-phase L encoding) with aircraft identification code Distress message every 50 s 121.5 MHz and 243 MHz 100mW min (+20dBm) Modulation 3K20A3X Audio sweep from 1420 Hz to 490 Hz Continuous transmission MECHANICS Material Moulded plastic Colour Yellow (colour compounded) Mounting bracket with velcro strap WEIGHT AND DIMENSIONS 1290 gr (2.84 lb) with battery, bracket and auxiliary antenna Housing: 172 x 82 x 82 mm (6.77 x 3.22 x 3.22) Over all dimensions (with auxiliary antenna): 285 x 107 x 993 mm (11.2 x 4.2 x 3.6) TESTS & CERTIFICATION Type AP ED 62, ED14, JTSO-2C91a, JTSO-2C126, TSO-C91a, TSO-C126 DO183, DO204, DO160 Resistance, crush, 500 G shocks, cabin depressurization, watertightness CONTROL PANEL ARM / OFF / ON switch Bright red LED BNC antenna connector DIN12 connector for remote control panel OUTSIDE ANTENNA (on option) Three frequency (121.5 / 243 / 406 MHz) Rod or Blade depending on the aircraft speed AUXILIARY ANTENNA Three frequency (121.5 / 243 / 406 MHz) Whip 400mm (15.75) BNC connector Tel. (+39) 06.363.04.761 - (+39) 06.363.04.941 Fax (+39) 06.32.97.337 KANNAD - ZI des Cinq Chemins - BP 23 - 56520 Guidel - France / Tel: +33 2 97 02 49 49 / Fax: +33 2 97 65 02 19 / contact.aviation@kannad.com Copyright 息 KANNAD. All rights reserved. The Kannad 406 AP has been specifically developed for quick operations when time means money: the housing is velcro mounted and programming can be done automatically by plugging a programmed connector (programming dongle on option) to the ELT front panel. This means that the ELT can be easily replaced on board within seconds. TECHNICAL SPECIFICATIONS Ref: DOC98099F The Kannad 406 AP is programmed with either the aircraft tail number, a serial number or the aircraft operator designator. As the ELT does not need to be opened, this operation only takes a few minutes and can be carried out inside the aircraft.