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LOCATION
ZONE: 127,128
COMPONENT DESCRIPTION
The face of the interrogator is fitted with a TEST
pushbutton switch and six LEDs.
- R/T OK (green): DME OK.
- R/T FAIL (red): DME faulty.
- BUS IN FAIL (amber): invalid input.
- ANT FAIL (amber): antenna faulty.
- IND No 1 FAIL: indicator No 1 faulty.
- IND No 2 FAIL: indicator No 2 faulty.
The back is fitted with an ARINC 600 connector.
TMUDMEF04-T03 LEVEL 3
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DME COMPONENTS - INTERROGATORS (THOMSON)
TMUDMEF04-P03 LEVEL 3
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DME COMPONENTS
DME ANTENNAE
IDENTIFICATION
FIN: 3SD1, 3SD2
LOCATION
ZONE: 121,127
COMPONENT DESCRIPTION
The DME antenna is of the blade type with a radiating
cavity driven by capacitance coupling.
It is vertically polarized and has an impedance of 50
ohms.
DME and ATC antennae are interchangeable.
TMUDMEF04-T04 LEVEL 3
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DME COMPONENTS - ANTENNAE
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34 - NAVIGATION
34-52-00 ATC SYSTEM PRESENTATION
CONTENTS:
Principle
Components
TMUATCF08 LEVEL 1
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ATC SYSTEM PRESENTATION
PRINCIPLE
The Air Traffic Control (ATC) transponder is an
integral part of the Air Traffic Control Radar Beacon
System (ATCRBS).
The transponder is interrogated by radar pulses
received from the ground station.
It automatically replies by a series of pulses.
These reply pulses are coded to supply identification
(Mode A) and automatic altitude reporting (Mode C) of
the aircraft on the ground controller’s radar scope.
These replies enable the controller to distinguish the
aircraft and to maintain effective ground surveillance
of the air traffic.
The ATC transponder also responds to interrogations
from aircraft equipped with a Traffic Collision
Avoidance System (TCAS) (Mode S).
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ATC SYSTEM PRESENTATION - PRINCIPLE
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ATC SYSTEM PRESENTATION
COMPONENTS
The components are two transponders, four antennae,
and one ATC/TCAS control panel.
Note: The TCAS/ATC control panels shown here after are
given as examples. They may differ according to
the aircraft configuration.
TMUATCF08-T02 LEVEL 1
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ATC SYSTEM PRESENTATION - COMPONENTS
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34 - NAVIGATION
34-52-00 ATC DESCRIPTION/OPERATION
　
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