In preparation for the switch being installed to control the electric fuel pump, the red wire that powers the fuel pump was removed from pin 29 of the fuselage connector using a pin removal tool. The plan is to install a new wire from pin 29 to one of the recently purchased rocker switches and hopefully have enough wire length to secure the removed wire which runs to the fuel pump onto the rocker switch without making any splices. At this point, it looks good .... the final switch position on the panel will be determined later after seeing how much room there is once all the panel goodies are installed.
Inserting the pin removal tool to release the fuel pump wire from position 29 of the fuselage connector.
The electric fuel pump wire with removal tool after the wire was removed from position 29 of the fuselage connector.
After the electric fuel pump wire was successfully removed from the fuselage connector, a replacement 18 gauge red wire was prepared. This new wire will run from pin 29 of the fuselage connector to the yet to be installed panel rocker switch for the electric fuel pump. The male and female connector pins can either be soldered or crimped … I chose to use a special crimping tool made especially for crimping these connector pins. The tool has four crimping fingers which push into the barrel of the connector pins. As the tool is squeezed, it creates four dimples around the circumference of the connector pin’s barrel … thus compressing the barrel onto the wire. It is very easy to use … insert a stripped wire into the barrel of either a male or female connector pin, place the wire and connector pin into the hole in the crimping tool until the connector pin bottoms out in the tool ... then squeeze the ratcheting handles until the handles release. Presto! A completed crimp.
Inserting the wire with pin into the special ratcheting crimping tool.Completed wire with the newly crimped male connector pin which will run from position 29 on the fuselage connector to the yet to be installed fuel pump rocker switch.
With the exception of installing the extra switch to power the left landing light, the wiring at the instrument panel end of things for the shielded cables being installed for the landing lights and the navigation/strobe lights is now completed. The two shielded cables were prepped and the 18 gauge wires were terminated with female pins and installed into the appropriate positions on the options connector. Unlike the fuselage connector, Van’s already shrunk the heat shrink around the wires going into the options connector. I did not want to make any cuts in the shell of the connector so decided to strip back the shielding on the two cables so the shielding ends just before the shell of the connector.
Stripping back the shielding with a pair of flush cutters.
Heat shrink tubing was placed over the separate 18 gauge wires for added protection where the wires enter the shell of the connector and also where compressed under the strain relief. A second larger piece of heat shrink was placed over the cables where the shielding was terminated to make a smooth transition.
Upper cable is the completed wire prepping. The bottom cable shows the heat shrink on the separate wires prior to sliding the larger piece of heat shrink over the transition area.
Female connector pins were crimped onto the ends of the four wires and the wires were inserted into their correct locations on the options connector … followed by reinstalling the connector’s shell.
The completed options connector with shielded cables installed for the navigation/strobe lighting plus the right landing light power and Wig-Wag power for both landing lights.
A separate 18 gauge wire was pulled through the wire grommets from the instrument panel to the electrical connector for the left wing. This wire will be connected to a yet to be installed rocker switch which will control the left landing light’s steady on power. This idea has been strategized in previous posts on the topic.