Kannad AF INTEGRA, Руководство по эксплуатации

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OPERATION MANUAL
AF INTEGRA / AF-H INTEGRA ELT
PAGE: 3
JUN 20/2013
2. KANNAD 406 ELT System Presentation
AF INTEGRA and AF-H INTEGRA belong to the AF type of ELTs which are
permanently attached to an aircraft. AF INTEGRA and AF-INTEGRA (ER) are
designed to be installed on fixed wing aircraft or helicopters. AF-H INTEGRA
and AF-H INTEGRA (ER) are designed for flat installation on board helicopters
only.
The INTEGRA ELT system ( Refer to Section Figure 2: ELT system description
page 4 ) is composed of:
1. the ELT transmitter:
• P/N S1851501-01 for AF INTEGRA (ER) or,
• P/N S1851501-02 for AF INTEGRA or,
• P/N S1852501-01 for AF-H INTEGRA (ER) or,
• P/N S1852501-02 for AF-H INTEGRA
2. a mounting bracket (P/N S1840502-01 or S1840502-02);
3. an external whip, rod or blade antenna;
4. A remote control panel
(1)
;
5. a DIN-12 connector, programming dongle or dongle IF GPS RS232
(2)
when the optional RCP is connected.
6. an outside buzzer (optional).
Note: (1) The RCP is optional only if the commands and controls of the
ELT are reachable and visible from the pilot seated position.
(RTCA DO-204A):
"Equipment control and indicator installed for in-flight use shall be readily
accessible from the cockpit crew position. The cockpit crew shall have an
unobstructed view of visual indicator when in the normal seated position."
Note: (2) GPS/NAV Interface with an on board RS232 GPS.
For details of approved part number of INTEGRA ELT system, Refer to Section
6. Compatibility list page 110 .
The transmitter and bracket are installed in the aircraft near the tail. The
external 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 DIN-12
connector or a programming dongle and a 2, 3, or 4-wire bundle (not supplied)