FWF wire routing routing progress

We re-ordered the coil packs to keep the cables a bit more organized:

Spark plug wires after changing the order of coil packs

I re-terminated the EFII ground lugs to use the ground tabs (and leave the larger bolt for the main engine grounding):

EFII ground wires connected to grounding block

After securing the sensor cables (oil pressure, oil temperature, fuel pressure, manifold pressure) inside the cockpit, I cut them to length and terminated them on the sensors - most of them were Metri-Pack 150 pull-to-seat connectors, which are slightly annoying since you have to crimp with the wires running through the connector:

Sensor Metri-Pack connector assembly

Sensor wires connected to FWF sensors

Oil temperature sensor connector

For securing the ignition and sensor wires around the cylinders, I couldn't find a bracket with the shape I wanted, so I 3D scanned the side of the engine and made one:

Spark plug wire bracket in 3D-scanned engine

Spark plug wire bracket design

A 3D-printed prototype showed that I had the right measurements off of the 3D scan, but it also seemed a bit flimsy, so I iterated to make a beefier version. Given the position of the injectors, I'm also not sure that top hole will be very useful:

Test spark plug wire bracket in place

Besides that, in favor of finishing the wiring behind the firewall, we organized, trimmed and terminated the alternator regulator wires that come from the FWF. This area is very annoying to access and I regret placing the regulators there already, but with some contortionism and a lot of patience, we got it more or less organized:

Original wiring mess near the alternator regulators

Wife doing contortionism to organize the alternator regulator wires

Slightly more organized wiring underneath the alternator regulators

We still need to replace the zipties with wax lacing and connect a couple more wires in that area.

With that side's lengths also set, I terminated the starter annunciator connection, with the inline resistor (installed in a Z shape with heatshrink, as the VP-X manual suggests), as well as the alternator field outputs:

Starter relay with all inputs connected

Next I'll make more of the spark plug wire brackets and finalize the rest of the FWF routing.

Time lapse:


Total avionics rivets: 181
Total avionics time: 401.4h

Flap motor secured

Very short post - after figuring out the heat tee servo installation, I secured the flap motor and its wires for good:

Flap motor secured in place inside the tunnel

With this, section 40 is complete.

Time lapse:


Total flap system time: 20.5h

Windshield installation complete!

We started work on the bottom windshield fairing, following the EAA method, by sanding the metal and the plexiglass, applying structural adhesive to the surfaces, then applying a small layer of filler to the joint (being careful to not let much of it go inside):

Windshield joint with sanded metal and plexiglass

Applying filler to windshield joint

Windshield joint with adhesive and filler applied

It was then time to apply the "fake prepreg" strips of fiberglass - a 2.25" strip with 2 layers of fiberglass. To make it easier to work with, we chose to split it roughly at the middle, with each layer being a couple inches offset to make an overlap near the center:

Laying up fiberglass on top of the prepreg plastic

Pre-pregging by squeezing the resin into every part of the fiberglass

Cutting the prepreg into 2.25" x 3.5' offset strips

Windshield joint fiberglass after curing

Once that cured, it was time to apply another layer of filler (a little thicker this time, meant to give it shape), followed by another couple layers of prepreg fiberglass:

Windshield joint after sanding the first layer of fiberglass

Patricia performing "precision guesswork", shaping the filler to follow a nice curve

Windshield joint with filler applied to its full extent

Windshield joint with a second fiberglass layup applied

The fiberglass overlap with the column needed some significant sanding to make a smooth ramp down to the door surface:

Windshield joint, sanded where it meets the column

It was then time to apply the Aeropoxy Light filler, which is a very thick but also very light paste:

Mixing Aeropoxy Light filler

Aeropoxy Light (with black tint) applied to the windshield joint

Sanding the Aeropoxy left some clear high and low spots, which were then filled with polyester icing, which was itself sanded and primed, then the primer was fine-sanded smooth, yielding a nice finished fairing:

Sanding Aeropoxy Light

Sanded Aeropoxy showing some high and low spots

Polyester icing applied to fill irregularities in the surface

Finished windshield fairing, primed and sanded

We also filled the gap behind the fairing where the windshield meets the cabin cover column, with black-tinted resin, to reduce the chance of future cracking of the fairing:

Gap between the windshield fairing, the windshield and the cabin cover column


The minor imperfections around the transition will become Jonathan's problem :)

With this, section 45 is finally complete!

Time lapse:


Total cabin door and transparency rivets: 147
Total cabin door and transparency time: 272.8h

Installing the windshield

After curing, the door windows were complete:

All windows installed in place

We started the windshield installation by carefully determining the centerline of the airplane, and matching that to the center of the windshield:

Using the laser to find the center of the fuselage, to align the windshield

That is, until we realized the center of the windshield is BS and totally irrelevant given the irregular shape :) and instead we simply adjusted it to a position that seemed to make more sense and look good, trimming the edges as we went until we got a gap of less than 3/32" all around the cabin cover flange. We then marked it and trimmed down to get the actual consistent 3/32" gap, using arbitrary markings to realign:

Alignment markings on the windshield and fuselage

Trimming the windshield with a sanding disk

We sanded the cabin cover flange until the fiber was exposed (same as for the windows), and did some more minor adjustment of the flange and windshield edges to keep a consistent 3/32" gap:

Fuselage taped up for sanding the windshield flange

We then taped up the windshield - the top following the Silpruf process, and the bottom following EAA's process:

Windshield with external tapes applied to it

Windshield with interior tapes applies to it

Fully-trimmed windshield held in place by clecos and clamps

With the window ready to attach, I also fabricated and attached the 5 clips that are supposed to hold it in place:

Metal clips for holding the windshield

Windshield held in place by metal clips

We then followed the same process as the windows' for the top edge of the windshield, applying Silpruf, installing spacers, waiting for 12h, then trimming the spacers and gluing it in:

Windshield with a first layer of Silpruf applied to the top edge

Windshield attached to the top flange with Silpruf

We had tried to keep the cleco holes relatively shallow to reduce the change of hitting the conduit behind them, and that worked fine initially but during that final attachment some clecos just didn't take - cleaning off the Silpruf around them and from the clecos themselves helped (I guess the Silpruf was acting as a lubricant and making the clecos slide out?), but we also added some clamps to lower the pressure against the clecos.

We also already marked the edges of the fiberglass fairing, which is what we'll tackle next:

Bottom windshield fairing space taped up for fiberglass layup

Time lapse:


Total cabin door and transparency rivets: 142
Total cabin door and transparency time: 257.9h

Door windows attached

After the Silpruf on the rear windows had cured, we removed the clecos, and they held!

Rear window attached in place, without clecos holding it

With this, we repeated the same process for the door windows, startin with trimming the windows and sanding the door flanges (only enough for the fibers to show):

Door window flange, sanded until the fibers show

We trimmed the windows to leave a 3/32" gap, then drilled those gaps for clecos (and unlike the rear windows, on these the holes did not go all the way through, which is convenient since finishing will be easier (no repainting the inside):

Right door window held in place with clecos, after trimming

We taped up the area where we didn't want Silpruf, and attached spacers with RTV:

Left door with protective tape and spacers glued on

A first layer of Silpruf is applied to the end, then let cure for ~24h:

Applying Silpruf to the door window edges

Spreading Silpruf into a thin layer on the door window edges

Right door window with Silpruf applied, and the first tape removed

We then apply a second thin layer of Silpruf to the window, and a thick layer to the window flanges:

Applying Silpruf to the right door flange

Right door window set in place with Silpruf, held at the right depth by clecos

Left door window set in place with Silpruf, held at the right depth by clecos

We had a bit too much squeezeout on some of the inside edge, and too little on other parts, so a lot of adjusting of the inside finish had to be done:

Cleaning up the excess Silpruf that squeezed out of the inside

After removing all the Silpruf-cutting tapes, the end result was pretty good:

Right door window installed in place, after the inside edges were cleaned up and the tape removed

With this, the only part of section 45 remaining is installing the (dreaded) windshield.

Time lapse:


Total cabin door and transparency rivets: 142
Total cabin door and transparency time: 242.5h