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TX56/56A and TX57/57A Installation Manual
5 April 2022
01776-00-01
Issue AD
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Page 4
Trig Avionics
2.2 Interfaces
At the rear, the Nav/Com unit has a 25 way D-type connector for the
communication radio and audio system, and a 44 way D-type connector for the
navigation receiver. There are two antenna connectors for blind mating with
the corresponding connectors in the mounting tray – one for the
communications radio, and one for the navigation receiver.
Note: A single antenna input is provided for the VOR/LOC and
Glideslope receivers. Many aircraft VOR/LOC antennas also provide
adequate coverage of the glideslope band, and a single antenna can
be used. Where the airframe or antenna arrangement precludes this,
an external antenna combiner will be needed to present both inputs
on the single connector.
The 25 way D-type interface provides the following services:
INPUTS
DESCRIPTION
Power input
The TX56 operates on 11 to 33 volts DC. The TX57
operates on 22 to 33 volts DC.
Lighting bus
input
Connects to the aircraft lighting bus and is used to adjust
the switch lighting intensity.
RS232 input
An optional input to allow preloading of frequencies,
generally from a GPS navigator.
Push-to-talk
inputs
There are two push to talk inputs corresponding to the two
microphones. For backward compatibility with older
installations both microphones can optionally be gated by
a single PTT input.
External flip-
flop input
An optional keyswitch input to enable remote transfer of
primary and secondary frequencies
Intercom
keyswitch
An optional input to allow the intercom to be switch
controlled.
Microphone
inputs
There are two microphone inputs, suitable for
conventional aircraft microphones.
Содержание TX56
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