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Here's mine. This is based on the AeroElectric Connections Z11 diagram. My engine is an O-235-C1. It does not have an engine driven fuel pump but uses two electric pumps. For this reason I have triple backup for power to my pumps. It includes an endurance bus and an always-on bus.
Note that I have an extremely low amp draw system. Typical in-flight electrical load is 4 amps total with lights off, If I put strobes and landing light on it jumps to under 8 amps. Obviously I don't have any glass in my panel except for a G5.
Also I wanted to avoid a key start switch to eliminate a point of failure. I start via a simple toggle switch. I produced my drawing in AutoCad.
Thank you Gary for your help by sending me this beautiful electrical diagram which will help me for my construction.
A big thank-you
Excuse me my english is not very good