Garrecht Avionik GmbH
VT-01 Transponder
Installation Manual - english -
Document:
01.0200.11E
Revision: 1.3
15
Replace the screws (4-40) in the back of
the central unit with quicklock terminals, if
installed
Rear view of central unit
1. Assemble mating pressure
connector and plug for both units
in the correct orientation
2. Push the steering unit (1) onto the
central unit (2) . Use the 4 screws
(3) to fasten both units.
6.1.2. Panel mounting
Determine a suitable position in the instrument panel that is in view of the pilot in command.
When choosing a position for installation, always be sure not to damage structural devices of
the airframe.
Cut a 57mm (2 ¼ inch) diameter hole with 4 x 4.1mm holes for the mounting screws (see chapter 15
for detailed locations). A minimum space of 65.5mm x 65.5mm behind the panel cut out is required for
clearence with adjacent instruments. A depth of 205mm is recommended to accomodate the
transponder and electrical connectors.
6.1.3. Static pressure connection
The system contains an integral alticoder. Connect the static pressure line of the aircraft to the
connector on back of the central unit.
Front of central unit
