INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AF / AF-H / AF (6D)
PAGE: 3
JUN 23/2008
2. KANNAD 406 ELTs Presentation
The KANNAD 406 AF / AF-H / AF (6D) are composed of:
1.
a transmitter;
2.
a mounting bracket;
3.
a remote control panel (mandatory if ELT controls are not available from
the pilot’s position, refer to RTCA/DO-183, RTCA/DO-204, EUROCAE
ED-62);
4.
an outside antenna;
5.
a "Programming Dongle" for pin-programming function (option);
6.
CS144 Interface Module (option).
The transmitter, bracket, Programming Dongle and CS144 Interface Module
are installed in the aircraft near the tail. The outside antenna is mounted on the
fuselage near the tail. The remote control panel is installed in the cockpit and
connected to the ELT with a 4 or 5 wire bundle.
Figure 2: ELT system description
The KANNAD 406 AF and AF(6D) are designed to be installed on fixed wing
aircraft or helicopters.
The KANNAD 406 AF-H is to be installed
only on helicopters
.
