Wired up the regulator/rectifier wires today. The regulator rectifier takes the 3-phase alternating current produced by the engine's built-in alternator and converts it to steady, 14.5 volt DC throughout the operating range of the engine. The positive (+) wire from the regulator/rectifier suppplies primary power to the aircraft's electrical system and charges the battery and is now attached to the output side of the Master Solenoid. The negative (-) wire grounds the circuit and is attached to the primary aircraft ground.
The wires will be tied down when I finish off the engine compartment wire routing.
Wires exiting regulator (sliver bracket with orange hose) enroute to Master Solenoid.
Regulator/Rectifier wires attached to Master Solenoid (lower) and aircraft ground (upper).