Panel Overhaul - Part II
After removing all of the old wiring and sensors, it was time to start installing the new wiring. I followed the guidance of two very knowledgeable authorities when it comes to wiring, Bob Nuckolls, and the FAA with "AeroElectric Connection" and "AC 43-13.1b" respectively. Coming from the automotive world where everything is shrouded in heat shrink, potting, and boots, I have really come to appreciate aircraft wiring. All aircraft wire is white (labeled at both ends), and all wiring bundles are constrained with waxed nylon lacing and adel clamps for complete serviceability.
Many of the sensors need custom mounting solutions, such as this fuel flow sensor. I machined a split clamp out of 6061-T6 aluminum. After it is mounted, insulation is installed to prevent the fuel from vaporizing.
After the wiring is run, it is labeled, cut to length, crimped with a pin or socket, and inserted in the connector shell. After all of the wires for a single connector have been run, the shields (green wires) can be grounded, the shell closed, and the wiring bundle laced for a secure trouble free connection.