I started today by bolting on the essential buss solenoid onto its mount. Then I bolted on the alternator regulators, fuel quantity adapters, essential buss diode and back up alternator current transducer. I also installed grommets in the fuselage side skin for the fuel quantity adapter harness to pass through. Lastly I reassembled the aileron control system and confirmed that there is no longer an interference between the aileron push rod and the aft spar pass through.
Essential buss solenoid bolted on
Alternator regulators, fuel quantity adapters, essential buss diode and current transformer installed
Aileron push rod aft spar pass through clearance resolved
