I’m getting ready to install the electrical system in my RV-8 and I was hoping you experienced builders could take a look at my power schematic and let me know if you see any issues. I based the design on Nuckoll’s Z-14. I fly IFR and wanted a dual isolated bus electrical system for several reasons. Each bus has its own battery and alternator/generator that runs all the time, and the devices are divided between the buses in a way that each bus has enough avionics to keep the plane right side up in the clouds and get me home.
By design, the only way to connect the buses is with the cross feed contractor and that will remain open most of the time. The goal of isolation is why I don’t dual feed the Garmin avionics that allow it or automatically use both batteries to feed the starter. I can always close the cross feed contactor if needed. The only connection between the two buses when the cross feed contactor is open should be the voltage sense feed from bus 2 to the GEA 24 on bus 1, which is the only way I could figure out how to monitor the voltage of bus 2 through the G3X system.
I have an IO-390-EXP119 / Whirlwind 300-3B/A-72 up front so I’m putting one PC-680 in the rear for weight and balance and another in the floor of the forward baggage compartment for convenience and to shorten the big wire runs. Each battery contactor is near its battery, and the battery contactors feed to the cross feed contactor inside the right gear tower. The bus bars and fuse box are located close together in the right console area, a short run away from their power source at the cross feed contactor. I have a B&C forest of trees ground block that attaches to both sides of the firewall and all grounds will terminate here except for the few grounds indicated in the schematic as being local or engine grounds.
One question that comes to mind--will having the forward battery’s ground terminal connected to the firewall ground bus while the aft battery’s ground terminal is connected to the longeron create any noise or other problems?
Please let me know your thoughts and if you see any problems that I have missed.

By design, the only way to connect the buses is with the cross feed contractor and that will remain open most of the time. The goal of isolation is why I don’t dual feed the Garmin avionics that allow it or automatically use both batteries to feed the starter. I can always close the cross feed contactor if needed. The only connection between the two buses when the cross feed contactor is open should be the voltage sense feed from bus 2 to the GEA 24 on bus 1, which is the only way I could figure out how to monitor the voltage of bus 2 through the G3X system.
I have an IO-390-EXP119 / Whirlwind 300-3B/A-72 up front so I’m putting one PC-680 in the rear for weight and balance and another in the floor of the forward baggage compartment for convenience and to shorten the big wire runs. Each battery contactor is near its battery, and the battery contactors feed to the cross feed contactor inside the right gear tower. The bus bars and fuse box are located close together in the right console area, a short run away from their power source at the cross feed contactor. I have a B&C forest of trees ground block that attaches to both sides of the firewall and all grounds will terminate here except for the few grounds indicated in the schematic as being local or engine grounds.
One question that comes to mind--will having the forward battery’s ground terminal connected to the firewall ground bus while the aft battery’s ground terminal is connected to the longeron create any noise or other problems?
Please let me know your thoughts and if you see any problems that I have missed.

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