Aquila ATO1, Руководство по обслуживанию

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MAINTENANCE MANUAL
AQUILA AT01
Aviation by Excellence AG
23-00-00
Page 01
Communications
30.04.08
COMMUNICATIONS - GENERAL
1.
A. This chapter describes and provides maintenance instructions to such components and systems,
which furnish a means of communicating from one occupant to another and between the aircraft
and other aircraft or ground stations.
B. Technical publications available from the manufacturer or vendor of the various components and
systems, which are not covered in this manual, must be utilized as required for maintenance of
those components and systems.
2.
A. The standard equipment of the AQUILA AT01 includes a Bendix/King KX 125 VHF NAV/COM
transceiver and an intercom system. The NAV/COM transceiver is mounted in the center of the
instrument panel over the transponder. The intercom control panel is located above the KX 125.
(1) That NAV/COM is for radio communication with ground control or other aircraft. In
addition, data of ground stations can be received and indicated for navigation purposes.
(2) The connection of the crewmembers headsets to the NAV/COM radio is provided and
controlled by the intercom system. It facilitates external and internal communication of the
crewmembers.
14 VDC for transceiver operating is controlled through the AVIONICS switch. The radio and the
intercom system are protected by the circuit breakers labeled “NAV/COM” and “Intercom”.
B. Optional to the Bendix/King equipment in combination with the PM 501 Intercom system, the
following NAV/COM equipment and Audio Panel combinations may be installed:
(1) GARMIN GNS 430 VHF COMMUNICATIONS TRANSCEIVER/ VOR/ILS RECEIVER/ GPS
RECEIVER in combination with a GARMIN GMA 340 AUDIO PANEL.
(2) GARMIN GNS 530 VHF COMMUNICATIONS TRANSCEIVER/ VOR/ILS RECEIVER/ GPS
RECEIVER in combination with a GARMIN GMA 340 AUDIO PANEL.
(3) GARMIN SL30 VHF COMMUNICATIONS TRANSCEIVER/ VOR/ILS RECEIVER/ GPS
RECEIVER with an integrated independent INTERCOM. This NAV/COM-Equipment may be
combined with a FLYMAP L Multifunctional Display and a GARMIN GI 106A CDI.
(4) GARMIN SL40 VHF COMMUNICATIONS TRANSCEIVER with an integrated independent
INTERCOM.
All listed devices are mounted in the centre of the instrument panel in the avionics column.
The 14 VDC power supply for the operating of the listed devices is controlled through the
AVIONICS switch. The NAV/COM portion of the GNS 430, GNS 530 or SL30, whichever is
installed, is supplied through a circuit breaker labelled “COM/NAV 1”, the GMA 340 Audio Panel
through a circuit breaker labelled “Intercom”. If the GARMIN NAV/COM SL30 or COM SL40 is
installed, the additional power supply for the independent INTERCOM portion of the device is
protected by a circuit breaker labelled “Intercom”.
Introduction
General Description