Landing lights and wing root fairings

Not much progress this week. I focused on switching out the connectors for the landing lights, and then installing the landing light lenses.

The original landing light wiring setup used molex connectors for the three wires providing power and ground to the Landing and Taxi lights. I was never very happy with the crimps on the wires, the poor connection, and the awkward angle of the wiring entering the molex connector.

I decided to replace them with DTM connectors, and re-route the wiring. DTM connectors provide better wire support, are water resistant, and have a much more positive connection and locking mechanism.

I removed the landing light clusters from both wings, brought them home and switched to DTM 3-wire connectors. Once I had them re-installed in the wings, I tested the lights and then installed the landing light lenses. The wiring setup is much more robust now, and I’m sure it will work out well.

I spent some time on the wing root fairings. Each fairing consist of two parts, an upper and a lower fairing. The upper is thicker and covers the area from the flap to just forward of the main wing spar. This is designed to be walked on when entering and existing the cabin. The lower fairing is thinner and longer, and covers the bottom of the wing, and wraps around the leading edge. Forming the curve around the leading edge was a bit time consuming. The plans explain the initial bend, which is easy enough, but then some careful manipulation by hand is needed to get the final shape. It took an hour or so to get the curve right on both sides.

There are a few more steps to finish these fairings, including riveting on a series of stiffeners.

Landing light bay with the new DTM connector visible.
Wing root fairings on the left wing. I was test fitting these, getting the bend right before installing stiffeners and dimpling holes etc
Bottom wing fairing where it bends around and forms the leading edge.

Trim System

I didn’t have much time this week, but I was able to get the trim system working correctly.

Using the laptop and a long Ethernet cable I was able to use the VPX configurator tool on my laptop to send power to the trim motors. I was pleasantly surprised that both the roll and pitch servos worked correctly. I carefully verified that the orientation was correct. It would be easy to reverse either one. For example, the elevator trim tab moves up and down just like the elevator, but it has the opposite effect from the elevator itself. Pitching “up” causes the elevator trailing edge to move up. Trimming “up” causes the elevator trim tab to move down, not up. It moves opposite the elevator, providing a force that moves the elevator to change the aircraft’s pitch.

After confirming the motors were working, I was able to set the correct max, min, and midpoint settings for both servos.

I then worked on mounting the aileron trim brackets on the right wing aileron pushrod. These connect the springs from the servo control arm to the pushrod, actuating the aileron.

Aileron trim servo. The servo mounts onto the access panel at this point. Springs will attach to the holes in the end of the arm, and extend to the brackets on the pushrod.
Diagram of the aileron trim system showing the springs and how they connect to the pushrod and servo arm
Using the laptop to run the trim motors and to set the trim limit parameters
VPX config tool. The whole electrical system can be configured and activated from the laptop. The blue Ethernet cable is a 50 foot cable that plugs into the VPX box behind the panel
Due to interference between the springs and the pushrod, I bent the servo arm to gain some clearance
Springs attached to the servo arm.
One last picture before closing this up. Note, the d-sub connector is safety wired together