Got a nice early start this morning before it got stupid hot outside. I managed to finish up all the ground terminations by 8:00, at which it was time to stroll across the runway for Sunday Coffee Club. That was followed by several hours working on a Helio Courier that was donated to the Waller County Aviation Museum. Finally, I got back out and finished up the cable lacing and securing in the ground bundle area:

 At this point, I decided it was time to work towards actually powering up the panel. There was still a decent amount of work to be done before that, mainly from a quality-control (read: avoiding release of the magic smoke) perspective. What I decided to do was to disconnect every avionics connector in the airplane, apply 12VDC to the fuse blocks (with fuses installed, of course), and probe every pin in every connector, confirming that only the ones that were supposed to have 12VDC had it. After all, I figured the most likely cause of magic smoke release was putting bus voltage somewhere it didn’t belong.

That bit of testing took some time and was pretty tedious, and I also did the same testing for good grounds, ensuring everything was kosher. I also built out coax cables for the com radio and GPS-175 – I didn’t want any chance of something being damaged by powering on with no antenna connected. But finally, I had the panel and avionics shelf in, everything in place, and the main bus block tied to the power supply. I looked everything over one more time – that’d be a lot of money to ruin – took a deep breath, and flipped the switch.

What I got was not what I expected at all. A couple units flickered on briefly, and one display showed a splash screen for a moment before going dark. Was this the normal boot sequence? Nope, another flash, another brief splash screen, nothing. This seemed indicative of periodic voltage drops from the power supply, and checking across the terminals with my multimeter confirmed it – the drops were large enough to be noticeable on a relatively slow-responding digital multimeter.

Strange – this was a 12A power supply, and by the book all the avionics together should draw under 6.5. But still, I started pulling fuses – maybe I just needed to shed loads a bit. I eventually got down to just the two HDX displays, but still got the same results.

A this point I gave up and went inside for dinner. After thinking it over, and chatting a bit on a phone call with my parents, I decided to try one more thing – bypassing the fuse blocks entirely, and trying to only power a single display. And here I finally had some success – the one screen was actually able to get through the boot sequence. Even so, the display was still flickering from time to time, so obviously this power supply is problematic.

At least now I know that both displays are functional. I didn’t get the full-panel “it’s aliiiiive” photo I was hoping for, but I guess one display lit up is still something:

So, where to go from here? I may see if a neighbor has a better power supply I can bother. I may also try adding a 12V battery in parallel to the power supply to try and smooth things out a bit – it’s not a perfect solution but maybe it can at least get me through some initial testing.

Started off today revisiting that countersink bit chunk that was tuck in the longeron hole. At first I wasn’t getting anywhere, but eventually instead of trying to drive the thing out, I got a fresh bit and tried using that to push the broken off part out from below…and it popped right out. Should have tried that a while back, I guess.

I still needed to finish the countersinking, but overnight I had a real forehead-slapping moment about this job. Yesterday I was trying to work out some really crazy ways of running the countersink bit by hand. I thought about trying to just run it in the angle drill, but was thinking of threading the countersink into my thread-hex adapter and then chucking that in the chuck adapter for the angle drill, and thinking that would all be too bulky. When I thought of it the way I just typed it, though, I realized my stupidity…I could just thread the countersink bit directly into the angle drill…duh. With that realization, I finished the countersinks and riveted the nutplate in no time, then got the adel clamp loosely attached, just to keep the wire bundle roughly in place.

Then it was time for some terminations. First was the short pigtail for the fuel pump – I’m using handshake splices for this connection. It occurred to me today that blade terminals might be nicer down the road, but I don’t have those in the right sizes, so handshakes it is. I needed to do the pigtail first because the fuel pump ground was the last wire to add to my bundle – I temporarily removed it while pulling the bundle through the gear tower. While working on this stuff, I also went ahead and laced the bundle up to and a bit past where the pump pigtail comes out.

Finally, there was nothing left to do but to start trimming and terminating the actual grounds. I got through eight of them (out of, I think, thirty-some) before calling it a night. These went pretty quickly, so I’m feeling confident about wrapping the rest of these up tomorrow – though there will be some pauses to handle lacing up the bundles. I want to go a little beyond just lacing the big bundle until it splits to individual ground tabs, maybe lace together batches of eight or so just to provide some vibration support closer to the tabs.

But hey, I finally have a photo again:

Another no-photo night, I’m afraid. I decided to work on making provisions for securing the ground bundle. I already knew I’d be adding an Adel clamp on the auxiliary longeron forward of the gear tower, but I was debating also putting one on the forward brace above where the bundle goes down into the tower. The latter would be similar to what I did with the larger bundle coming up out of the right gear tower; on this side, the bundle was much smaller, but eventually I decided I wanted it secured as well.

Getting the nutplate mounted on the brac was pretty straightforward, though it still required the angle drill and some other creativity. The longeron was a lot more fun – initially I thought about just drilling the screw hole and using a nut instead of a nutplate, but I really didn’t like the idea of needing two hands to get the thing secured, so I went with the nutplate mount here too.

Unfortunately I didn’t finish that mount. The aux longeron is kinda fun to work on since it butts against the curved forward side skin – this means getting a tool aligned with a hole can be challenging. I already knew I’d have to make the rivet countersinks by hand, but I couldn’t even use the long shaft with the countersink bit here. Eventually I rigged up a combination of a hex adapter, 1/4” socket, wobbly joint, and a few extensions. That worked but it seemed like it’d take forever. So I added an adapter and my T-handle wrench, which let me put more torque on the setup.

That turned out to be a bad combination – it was hard to keep the bit well aligned, but easy to overcome the resistance from bad alignment with the T-wrench. The result was that I snapped the tip off my countersink bit on the second hole, and that tip remained lodged in the hole. I worked on extracting it for a while but eventually decided that I was getting to the point of causing damage if I kept trying to force the issue. Hopefully revisiting this in the morning, I’ll have better luck.

Just a brief session tonight. Earlier today I sola fantasized about getting all the ground terminations done tonight and powering things up before the weekend, but it didn’t take much looking out in the hangar tonight to realize that was hilariously optimistic.

I got the newly-laced bundle pulled down into the gear tower and through the hole towards the firewall – kind of a pain really since all the masking tape tags made it impossible to just feed the bundle through as a unit. Between that and feeding a snap bushing over the end of the bundle to put into that hole, the result was a pretty tangled bunch of wires that needed some attention.

Next I sat down with the label printer and went through all those wires, putting in the labels for them. Kinda fun keeping track of which of 30-some wires I have and have not typed in already. Plus there were a couple tape labels that I was no longer sure what they referred to, so I ended up referring back to the schematics a couple times, just to make sure I was labeling things properly. Then I printed out a loooong string of heat shrink.

Before I trim anything to length, I want to get an Adel clamp mount point into the auxiliary longeron, since this bundle will need securing. That’ll let me get the general routing of the bundle down pat, and then I can start thinking about trimming. It’s going to be fun doing this since the area between the gear tower and the firewall is a bit snug.

Alright, time to start thinking big-picture. Electrical stuff is fun and all, but I need to start thinking about working on the canopy at some point. This matters because the brittleness of Plexiglass is directly related to temperature – the warmer, the better. Basically, I don’t want to find myself starting on canopy stuff when it’s getting colder outside (of course, “cold” in Houston is very relative).

So what I’ve been thinking is that I want to get most of the electrical stuff behind the panel done, and then pretty much pause that work and move on to the canopy. Practically, my general plan is to get the ground terminations done at the firewall, do a final inspection, and do the ceremonial first power-on of the panel. Once that’s done, then I’m going to break out the Plexi.

Tonight I was looking at the grounding. First up was getting the ground bus block installed on the firewall. This block provides a bunch of 1/4” tabs on the interior side for my individual grounds, and a big fat lug on the firewall side for grounding to the battery. Practically, mounting it is easy, but I’ve spent a lot of time worrying about inadvertently putting it somewhere that will cause problems down the road when I get to working on FWF stuff. But after a lot of studying the FWF drawings, I decided on a spot and did the deed tonight.

Interestingly, as provided the block only provides one usable mount hole, where the big ground lug goes through. I didn’t feel this was enough for secure mounting, so in addition to the main lug hole, I added a smaller hole at the other end, where a #6 screw and nut keep the thing from rotating. So now I have the bus block mounted in place:

Next up was looking at the routing of the big bundle of ground wires. I laced this bundle up on the bench a while back, but like a lot of the lacing work from then, things seem loose – the individual laces like to move around. So as I’ve done other places, I pulled the bundle out of the gear tower and re-laced the whole thing. With that done, I should be able to get it in its final routing next time out, and start doing some terminations. None of this will be too complicated, but there are a lot of wires, so I’m just going to be doing a bunch of trimming, labeling, and crimping. Plus there’ll be a bit of work figuring out how to secure the bundle, but I have a pretty good idea how I’m going to approach that.

What to do next? I feel like I’m in a weird state where I have plenty of small things to do but somehow it’s hard to decide which to work on at any given point. Well, tonight that thing was the OAT (outside air temperature) sensors. The Dynon OAT sensors connect to the ADAHRS units; this is why I have two to install (one per ADAHRS).

I’ve been sort of thinking for a while about exactly where to locate these. Some folks really like to put them out on the wings, but I didn’t want to deal with the wiring to make that happen. Second-best choice seems to be back at the tail. In this area, there seem to be two locations that people use; the first is on one side of the fuselage, under the horizontal stab, the other is on the aft most bulkhead, so the sensors are inside the empennage fairing.

I kind of liked the first idea from the perspective of keeping the exterior of the aircraft clean (plus not drilling more holes in my skins), but there are a couple potential issues with that spot. The first is that as the name of the sensor indicates, it really is supposed to go outside the aircraft; the idea is to read the ambient air temperature. Arguably, the area inside the empennage fairing isn’t really getting warmed by anything, so the difference might be trivial in most aircraft, but I expect to have the tail painted a dark color, which means there’ll be a good chance of significant solar heating of this area.

So it seemed that outside was the place to go. Next question, where back here? My strong desire for symmetry made me want to put one sensor on either side of the fuselage, but I didn’t like the consideration of dealing with the wiring for this – specifically routing one pair of wires from one side to another, in a way that it wouldn’t have a chance of interfering with the elevator push tube, which will pass through here. So instead I just put both sensors over on the right side.

That just left making the holes; laying them out far enough down to be away from the longerons, and properly spaced apart. Next was feeding the wires for each sensor through the hole, then feeding the nylon washer and nut from the backside and getting the sensors snugged in place:

Then I fed the wires forward, where they’ll run alongside the elevator trim and tail light wires. A look at the backside of the sensors through the aft deck:

Then I got to re-lace the wire run I put together a while back, adding the OAT wires to the bundle:

Next up I’ll need to get these terminated at the ADAHRs units. Which is another decision point; both sensors came with a lot of wire, pre-terminated with micro Molex pins. So I have a choice of either retaining the full provided wire length, which means coiling up and properly securing several feet of extra wire, or trimming and re-terminating the wires…assuming I even have the micro Molex pins on hand. I think I do, but I’m far from sure, and I didn’t check before coming in for the night. I’m leaning towards the latter just because my desire for neatness will be offended by coil of wire just sort of hanging around.

Another thing I did tonight was to finally commit to removing my fuselage rotisserie fixture. After thinking it over a lot, I don’t think I’ll need to roll the fuselage over again, and I want to have access to the firewall so I can start working on stuff there. First and foremost will be getting the ground bus installed and doing all my ground wire terminations, but there’s also adding the wiring passthrough hole on the right side. Once that’s done, I can pull through the harness bundle, then feed the ignition coil connectors back through into the cabin, and finish lacing up the harness section that’s waiting on that bit.

All that is to say, here’s the first look I’ve had at the bare firewall in quite some time:

Since I finally got in the parts I needed from Mouser, I figured tonight I’d revisit the switch console where I got hung up a while back. I got the sockets all installed in the plug housing, and did a test fit with the console. So now it’s all hooked up:

While working on that, I noticed how some of the lacing on the harness trunk along the baggage bulkhead had moved around. I think when I originally did the lacing on the harness, I didn’t really snug the stuff down very well, or else the bundles tightened up while being moved and installed. In any case, I decided to redo some of that lacing where it was clearly too loose. For all I know the new lacing might move around eventually too, but at least it looks better for now.