Kannad AF INTEGRA, Руководство по эксплуатации

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OPERATION MANUAL
AF INTEGRA / AF-H INTEGRA ELT
PAGE: 103
JUN 20/2013
The buzzer operates during the self-test procedure.
After about 10 seconds, the test result is displayed on the visual
indicator as follows:
• One long flash indicates valid test.
• A series of short flashes indicates false test result.
The number of flashes indicates the type of failure:
• 3 + 1 = LOW BATTERY VOLTAGE.
• 3 + 2 = LOW TRANSMISSION POWER.
• 3 + 3 = FAULTY VCO LOCKING (FAULTY FREQUENCY).
• 3 + 4 = NO IDENTIFICATION PROGRAMMED.
• 3 + 5 = FAULTY VSWR (LINK TO EXTERNAL ANTENNA).
• 3 + 6 = INTERNAL GPS SERIAL LINK.
It is recommended to test the ELT regularly in order to detect any
possible failure (
Refer to Section A. Periodicity page 301 ).
The number of self-tests carried out is recorded. This information is
available when the ELT is connected to a programming and test
equipment (PR600).
(3) Armed
In order to enable activation by the G-Switch or with an optional 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 except when the aircraft is parked for a long period or for
maintenance.
(4) On
This mode is selected:
• manually by switching the ELT to "ON";
• by switching an optional Remote Control Panel switch to "ON"
(provided that the ELT switch is in the "ARM" position);
• automatically when a crash occurs (provided that the ELT switch is in
the "ARM" position).
When this mode is selected, the ELT starts transmitting:
• after 50 seconds on 406 MHz (one 406 MHz burst every 50 seconds)
to the external antenna;
• after the GPS lock on 121.5 MHz (continous transmission between