INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AF / AF-H / AF (6D)
PAGE: 104
JUN 23/2008
programming and test equipment (PR600).
C. Armed
In order to enable activation by the G-Switch or with the Remote Control Panel,
the ELT must be in standby mode with the switch in the ARM position.
This mode is mandatory during flight
. The ELT should remain in the ARM
position all the time except when the ELT is removed from the aircraft or if the
aircraft is parked for a long period or for maintenance.
The Remote Control Panel is energized by the ELT when the ELT’s Switch is
in the "ARM" position.
D. On
This mode is selected:
• manually by switching to position "ON";
• by switching the Remote Control Panel switch to "ON" (provided that the
ELT switch is in the "ARM" position);
• when a crash occurs (provided that the ELT switch is in position "ARM").
When this mode is selected, the ELT starts transmission:
• on 121.5 MHz & 243 MHz immediately (continuous transmission);
• on 406 MHz after 50 seconds (406 burst every 50 sec during 24 hours).
The red visual indicator on the ELT (and on the remote control panel if installed)
flashes and the buzzer operates.
In case of accidental activation, the ELT can be reset either by switching it to
"OFF" or by switching to "RESET" on the Remote Control Panel.
The number of 406 MHZ bursts effectively transmitted is recorded. This
information is available when the ELT is connected to a programming and test
equipment (PR600).
