HIC wiring
Reading the installation manual and the SI-PAC012 today, I learned that I have had a misunderstanding of the engine controls and fusebox. Since the harness has connectors for the fuel pump power, I wrongly assumed that the HIC fuel pump connections for the fuel pump switches were simply control inputs that triggered either a relay that powered the pumps or triggered the ECU to control a relay.
However, it appears now from the current listed in the HIC table, that the power for the fuel pumps, the lanes and the start relay actually pass through the HIC to the switches and thus 16 gauge wire much be used rather than the 20 AWG I currently have in my wiring diagram. Since the SI-PAC-012 lists 10 of the large size contacts for the fuel pump wires, but I see need for only 4, I assume the other 6 are for the lane select switches and the starter relay switch.
If I am not understanding this correctly, please let me know. This architecture has this old EE scratching his head as I certainly would never design a system this way.
The logic of running the full fuel pump current through the HIC to the panel switches and then back to the fuse box before going back through the firewall to the fuel pump escapes me. I am rethinking now that I really don’t need to use the harness fuel pump connectors, but rather just power the pumps directly from my panel switches since they will carry full current anyway and are located in the mid-section of the airplane. Though, I probably will use relays as I prefer to keep switch currents at 5 A or less for switch longevity.