6 WIRING LOOM
The wiring loom of the RES is connected in parallel to the normal aircraft wiring loom. The
control system RES is powered by the two avionic batteries installed in the aircraft. There is
also a standalone fire warning system. The various electrical components should be wired
according to the wiring diagrams illustrated below.
NOTE: Each wire has a wire number that can be traced to the origin and destination of
the wire.
Display And Control Unit (DCU)
The DCU is located on the instrument panel within the cockpit of the aircraft. The DCU is
responsible for the human-machine interface.