Tailcone closeout stuff

Tonight I picked up with the intent of working towards getting the elevator control system reinstalled. In all probability this wouldn’t be the last time, but to my way of thinking everything from the bell crank back at least ought to be able to stay in place. First up, though, I needed to finish up work back where the ADAHRS units were, specifically routing the pitot/AOA lines and securing them for good.

This was kinda fun, all in all I think I removed and replaced the backboards back in the tail at least twice. I needed them out of the way to initially route the lines back from the seat floor area, but then of course needed them back in place to crawl back into the tail again – except there was one issue, with the way the lines were going to route up the bulkhead, the next-to-aftmost board had to be left out. I could only hope that I wouldn’t need to be that far back.

After putting the boards back and collecting the hardware and tools I needed for the adel clamps, I squirmed back into place to where I could reach the ADAHRS. One thing I wanted to do before buttoning things up back here was to double-check the electrical connections, and this turned out to be a good call. Both the D-sub network connectors were snugged down (I figured the most likely thing would be that I didn’t tighten the thumbscrews), but when I gave the OAT connectors a pull test…a wire came out of one of them. I was kind of expecting to have a bare wire come out – which would have been really fun – but it turned out the pin just hadn’t been seated in the connector. I just had to pull the connector and reinsert the pin, which would have been dirt simple any other time, but here it took about 15 minutes thanks to the cramped space.

Finally, I got back to the pitot lines, first inserting them into the connectors, then pulling the slack back forward and installing the two adel clamps. This, too, was made rather enjoyable thanks to the location. In some ways it was more fun than the connector – instead of lying on my back and reaching over my head, as it were, I was on my side and trying to use a screwdriver in one hand and a wrench in the other.

Once the adel were in place, I crawled out, removed the backboards again, pulled all the slack forward, and secured the lines to the aft bottom skin where I added a zip-tie pad – this will ensure the lines stay well clear of the rudder cable. The lines are visible in the lower right of this photo, and the red silicone tape can just be seen at the zip tie pad:

Next, I went to work on the control system. I decided to basically work through the entire fit procedure again, to make sure everything was still adjusted correctly. This meant installing both sticks on the control column on the bench, adding the pushrod between them, and making sure both sticks were parallel. Then the sticks came out again and I got the control column back in the fuselage, and the sticks and intermediate pushrod reattached yet again.

Next were the other two push tubes. A while back I disassembled these and gave them a coat of epoxy primer, after the rattle can primer got scraped up a lot just with the previous fitting work. The smaller forward push tube just gets set to a specified length, so I readjusted the rod ends, tightened the jam nuts, and added torque seal for good measure. This was about the time I decided I wouldn’t be installing the tubes tonight – I’d like for the torque seal to dry first, But I did pull down the larger aft tube as well, and reset the rod ends to where they were before (I took notes on this). This should be the proper length, but I’m not going to torque-seal these rod ends until I’ve verified the length…which will happen another day.

So that was the night’s work. I should be able to finish double-checking this stuff this weekend, and get it installed for good. The only complication I need to consider is the autopilot pitch servo – I need to review those installation instructions and see about getting that permanently installed at the same time I do the bell crank.

Posted in Fuselage | Hours Logged: 2

Finished attaching the horizontal stab

No time for a real session tonight but I figured I’d go try to get that last bolt in just for fun. Seems like it often works this way, but this time I got it started in the hole from below on the first try. The only complication was that it was a snug fit – not sure if the spacer between the aft deck and the stab was slightly misaligned or what. This was good in that once I got the bolt started, it stayed there, but bad in that I couldn’t get it pushed all the way through with my awkward hand positioning.

So I grabbed myself a ~2’ piece of scrap wood, crawled back into the tail, and was able to reach way back and get the bolt tapped all the way through, without having to even go horribly far back. Then it was pretty easy to get the nut on from above and get things torqued. So as of now the stab is officially permanently mounted.

I wouldn’t mind moving right on to adding the vertical stab, but I want to get new bolts to attach it – I think I mentioned last night that I decided to use all-new hardware for final-mounting the tailfeathers. This is a requirement anyway for the lock nuts, but I decide to go one step further and use virgin bolts as well. It’s cheap insurance for flight-critical attach points.

Maybe tomorrow I’ll start removing the back boards in the tail and get the elevator control system back in place.

Posted in Empennage, Fuselage | Hours Logged: .5

Changing course and working on the tail

So…after thinking over my next move quite a bit, I’ve decided to change up what I’m working on. Originally my plan had been to try and get the canopy cutting done this fall, before winter set in. The idea there is that cold temperatures increase the chances of cracking the canopy ($$$), and I figured otherwise I’d likely be getting to the point of canopy work sometime around the coldest part of the year. Thing is, at this point I’m a good month or more behind where I thought I might be, so rethinking things isn’t totally out of line.

What really pushed me in this direction was considering what I’d need to do to work on the canopy bubble. Broadly, there are two parts of the cutting portion of the program: first, the entire bubble gets progressively trimmed until it fits on the fuselage and frame correctly, and second, the bubble gets cut into two pieces, forming the windshield that gets affixed to the roll bar and forward upper skin, and the bubble that get attached to the sliding frame.

After doing a decent amount of reading on this work, one thing I really want to do is to attach the uncut bubble to the roll bar before cutting, to better ensure a really good fit. But I can’t do that until the forward upper skin is permanently riveted in place, and I’m nowhere near ready to do that. So that means either I don’t attach the bubble beforehand, or I don’t make the big cut right now.

Even setting that decision aside, no matter what I do right now I still have to put the canopy back in storage for a while after trimming and/or cutting. And honestly, I think I’d feel better just storing it as-is instead of after trimming, when I feel like it might be even a slight bit more prone to cracking unless I support it really carefully. Bottom line, I don’t think there’s a real need to try and rush into the canopy work right now, and I don’t see myself making such rapid progress that I’m at a point where I need to be cutting it any sooner than, say, next March, maybe later.

So, what to work on instead? I could pick back up with the wiring inside the airplane, maybe working on the stick grip wiring, but I think I need the control column in place before I can really do that, and with that installed getting in the fuselage and moving around is a little tougher. Instead, I decided to start thinking in terms of closing stuff out at the tail and working my way forward. This means permanently attaching the empennage, reinstalling the elevator control system, and maybe even moving on to fiberglass work, depending on how things progress with my engine order.

So that leads me to tonight. I figured I’d try and work on really attaching the horizontal stab, but first I needed to remove it again. I never did permanently install the two elevator control stop pieces I worked on a while back, and getting that riveting done would have been somewhere between difficult and impossible with the stab mounted. So I pulled that off, set it aside, and got the two stop pieces riveted (and, in the case of the aft stop, bolted) in place.

Next, I reinstalled the stab, this time inserting brand new bolts that I ordered specifically for final installation. The four bolts that attach the rear spar to the vertical stab bars were easy enough to torque, but the four bolts that drop in through the forward spare and down into the fuselage are another matter. Torquing these, I think, has to be a two-person job, with one person working inside the tailcone. If I contort my hand really carefully, I can touch the bolts inside the fuselage, but doing anything like starting the buts or operating a torque wrench isn’t happening.

I did decide, however, to see about crawling back into the tail and at least starting the nuts. I was under the impression that accessing the bolts that way would be no fun at all, but it turns out to be physically impossible as far as I can tell. I could probably do it if the ADAHRS mount wasn’t back there, but that’s riveted in place now and removing those rivets would be tough to do without causing damage. So I think I’ve got no choice but to find/bribe a very small person to crawl in there and help me out with this.

So that’s where I finished the night. Thing is, I’m kinda stuck until I get those bolts installed, since the next steps I’d be taking would involve adding even more stuff back there, and probably starting to remove the backboards that I lay on while crawling into the cave. Or maybe I’ll try going back out, inserting the bolts from below, and installing the nuts above. That might be doable, and wouldn’t require trusting, say, a neighborhood kid with properly torquing fasteners that attach an extremely critical piece of structure.

We’ll see, I guess.

Update: Well, my idea worked out fairly well. I was able to get three of the four bolts inserted from below, working through the aft deck, and I got those four torqued as well. The last one is proving to be a real bear to get the bolt inserted – that’s the hardest part. If i could get that done I’d be pretty much home free. Maybe I’ll give that one another try tomorrow evening, for tonight I’ve had my fill of contorting my arm and wrist.

Posted in Empennage, Fuselage | Hours Logged: 3

Finishing up canopy frame stuff

Picking up where I left off yesterday, today I got to work finishing up those side rails. I clecoed the rails back on the fuselage so I could mark the trim at the aft end, then removed them again to get the trimming done. Nothing special here, I just roughed the cut on the bandsaw and then went to work with a file to finalize things. Making the relief cut for the aft screw heads was a bit more fun. At first I tried just filing the relief cuts, but quickly decided that would take about half of my remaining lifetime. Instead I did the rough cutting with the Dremel and a rotary file, then just used the hand files to finish up the shape of the cutouts.

Here, you can see the relief cuts, as well as the slight taper from the trimming:

Then it was just a matter of getting the rails screwed in place on the fuselage. Next up was the anchor block back behind the rear seat; this was the only remaining component that wasn’t attached to the airplane yet. The anchor block just attaches with two screws through the back seat bulkhead. The location of the two holes is specified relative to the anchor block itself, but they actually get drilled through the bulkhead first, so a little math and thinking is required to get the layout right.

Next, the block needs some more work: on the forward side it needs to be countersunk to accommodate the dimples in the bulkhead, and on the aft side it needs to be counterbored for the attach nuts. Since the receptacle area is pretty right, the nuts get pressed into the counterbored holes and become captive nuts. The counterboring part was a bit interesting; I’d seen another builder mention that the specified 1/4” depth wasn’t enough, and I saw the same thing. Going 1/4” deep doesn’t even allow the screws to engage the nuts when inserted into the block, much less with the additional thickness of the bulkhead in play. So I went up to 1/2” instead.

The fun here is that the nuts need to be pressed beyond flush. Getting them started was pretty easy using my vice, and to press them further in I picked a small socket from my wrench set that fit nicely inside the hole. This worked great for one nut, but the other one turned sideways somehow, and I had to drive it out with a punch and start over again. On the retry, I pulled the nut into place using a longer #6 screw instead of using the vice; this ensured that it went in straight.

So here’s the back end of the finished anchor block, turned upside down mainly so it looks more like a funny face:

That just left dialing the bulkhead, which was definitely easier said than done. None of the squeezer yokes I had would work in the tight space, and I was kind of at a loss as to how to proceed. At one point I was really considering putting the dimple dies in place and trying to squeeze them between the jaws of a big pair of pliers, but fortunately I didn’t go through with that…I think I might well have damaged stuff that way.

Finally I came up with an idea. The problem here is mostly with figuring out how to handle the female dimple die inside the receptacle…but really I just needed something in there with the right shape. For example…the anchor block itself. With the countersinks made for the flush screws, I thought it might just do the job of the female die. So I dropped it back in place, closed the canopy frame to lock it in place, and installed one of the screws for good measure. Then I stuck the mail dimple die in the arbor of my C-frame, lined it up on the hole, and gave it a good couple whacks. The resulting dimple wasn’t perfect, but no worse than what I usually get out of pop rivet dimple dies (which would have been the other option here, and I would have had to buy a #6 set). A little work with the #6 countersink made everything all right, and then I repeated the job with the other hole, then finally installed both screws.

With that, I now have a fully functioning sliding canopy frame, with the exception of the latch, which will come later. And I now really have nothing else to do but to start working with the actual canopy bubble. To prepare for that fitting, I got out the forward upper skin and clecoed it in place again. I’ll likely have to remove some of these clecos to accommodate the actual bubble, but that I’ll just figure out on the fly.

In the meantime, I have an even more airplane-looking device sitting out in the hangar:

Posted in Canopy | Hours Logged: 3.5

Fitting the side rails and tweaking the canopy frame

So the goal for today was to get to the point of finalizing the placement of the side rails. Getting this done required doing some work with the frame itself to get the fit correct. The main goal was to get the sides of the frame to line up properly with the fuselage sides; this will ensure that the canopy skirt pieces fit nicely down the road when that time comes. The fit here is checked by cutting some thin strips of scrap aluminum, curling them a bit to match the curvature of the frame, and clamping them in place so their fit against the fuselage can be evaluated. With this done, we get a setup like this:

The previous photo was actually taken after frame tweaking, which is why the strips are fitting nicely against the fuselage. At first, though, the frame was a bit too wide, and the strips didn’t quite make contact with the fuselage, which meant I needed to squeeze things together a bit. The force for this was provided by a ratchet strap across the hoop at the front of the frame, but the other thing I needed was some way to reliably visualize how much I was bending the frame. This has more to do with the bending operation than the final dimensions of the frame, which can just be checked by re-checking the fit of the strips.

But for the bending portion, what I wanted to be able to do was to pull the frame to a certain point, relax and check the fit, and then pull it just a bit further on the next iteration. So I needed a good indicator for this purpose, and I went with a yardstick positioned across the top of the frame a little ways back, and clamped on only one side. To ensure precision, I put strips of masking tape on each frame and drew reference marks. The resulting setup:

After several iterations, I had the fit I wanted, with the strips just barely making light contact with the fuselage sides. At this point, I started making preparations for drilling the mount holes in the canopy rails. There are two prepunched holes towards the aft end of the rails, which get drilled from below, but the other four holes get laid out on the rail itself and drilled from above.

This was a spot where my level of trust in the plans was a bit on the low side. Not that I thought they were wrong, but more that it wasn’t quite clear where the reference point for measuring was, and it seemed a good idea to really understand where the rail mount holes would end up on the fuselage. The longitudinal measurements are made from the front of the rail – but my question was, did this refer to the very front of the rail, or the relief cutout I made to fit around the roll bar base?

The first hole was to be set 2 1/16” back; measuring from the back of the roll bar base put this hole just behind the joint between the aft spar carry through bulkhead and the canopy rail mount on the fuselage, which seemed like the right idea. But continuing to measure backwards, the third and fourth holes clearly needed to be positioned around the seat back support bracket – and starting with the roll bar base put the third hole obviously in conflict with that bracket, while the fourth one had lots of extra room.

This indicated to me that I should be measuring from the front of the rail instead; doing this moved all the holes forward by about 3/8”. Measuring this way, the third and fourth holes ended up nicely positioned around the seat back bracket, but now the first hole seemed to interfere with the carry through bulkhead joint. This seems wrong and baffled me for a good amount of time, but after evaluating the layout a bit more, I realized that the lateral position of the hole put it almost exactly between two of the attach rivets – which are spaced kinda far apart. OK, this was starting to seem a bit more reasonable.

Still, I was unsure, so before committing to anything, I went in and did some research – which yielded absolutely nothing. That is, no one saying “oh yeah this is how it works” but also not “oh no no no don’t do that.” That was enough for me to decide that the intent of the drawing was for this screw hole to go through the bulkhead flange.

So I drew the hole layouts on the bottom of the rails, intending to drill those pilot holes on the bench and then use them as a template later on. But before that, I laid each rail in place to recheck that the hole positions appeared rational. The only tweak I made from this fit-up was to adjust that first hole forward a bit, in order to have it land directly in line with the rivets in the bulkhead. To do this, I just laid a ruler along the rivet centerlines and under the rail, and drew a new mark to adjust my hole layout (the mark hasn’t yet been drawn here):

And so I finally got my mount pilot holes drilled in the rails…but then while reviewing he construction manual, I realized I wasn’t done tweaking the frame itself. The one adjustment left to be made was to get the proper vertical distance between the aft tip of the frame and the center slide rail. I figured this was unlikely to tweak the width of the forward end of the frame, but better safe than sorry.

The called-for spacing here is 5/8-3/4”, and I was well in excess of that. With a piece of 3/4” MDF on the rail, there’s still a good inch and a half of extra space:

To do the actual bending, I screwed a piece of scrap lumber into the tabletop, using a couple of 3/4” spacers to create a nice gap in the middle, with the entire apparatus spaced a few inches shorter than the length of the back end of the frame. This allowed me to tuck the aft end under the lumber and simply push down on the forward end of the frame to get my bending done. I would have preferred something more controlled, like I did with spreading the forward end, but I couldn’t figure a way to really do this with controlled force. Instead I just sort of estimated where the frame was sitting relative to my body while bending.

Here’s a look at the bending “jig:”

Also, rather than doing a lot of installing/removing the canopy to check the fit, I instead did measuring off the table for the rough bending. I already knew how much I needed the aft end to come down, so I set the frame on the table, measured the vertical distance from the table, and figured the new height I was going for. After a couple bending iterations, I was getting close and so I verified the fit on the fuselage before doing the final tweaking. It all ended up working quite well and now I’ve got a much nicer gap from the center rail:

After a final double-check of the fit – as I’d figured, the front of the frame still fir just fine – it was finally time to clamp the rails in place and do some drilling. This is kind of fun because it’s a little hard to work out a clamping strategy. Notably, the manual says you can also tape the rails in place, but that just seems nowhere near accurate enough. I ended up with a C-clamp at the back of each rail, and another about 6” back from the front end.

To position the rails for clamping, I started with the frame nearly full-open – just far enough forward that I could still get the clamps installed (once in, m the clamps would block movement of the frame). I got the rails set an equal distance in from each side of the fuselage, and with the rollers roughly centered, and clamped the back ends. Then the frame went forward and I repeated this exercise up there.

As a final sanity check, I measured the distance across the rails at a couple different spots. This showed that the front ends were about 1/8” further apart than the backs, so I did a little more adjustment of the spacing. I really would have preferred to be able to run the canopy through the full range of motion with everything clamped in place, but that simply wasn’t possible. In the end I just had to measure multiple times and then just kind of go for it.

Drilling started by taking the existing #40 holes (the four I drilled in each rail, plus the two prepunched holes in the fuselage) and using them to drill into the mating piece. The holes laid out in each rail were easy; the other prepunched ones were a little more fun. Those required laying inside the fuselage in various uncomfortable positions while wielding an angle drill (for the forward pair) and a cordless with a 12” bit (for the rear pair, which sit really close to the bulkhead behind the rear seat).

It was only after drilling all these initial holes, adding clecos as I went, that I finally got to test the full motion of the frame. Whew…no binding. That was a bit nerve-wracking.

Next, I needed to create access holes for the rearmost hole in each rail. All the other screws sit outboard on the flange of the rail, and are easily accessible from above, but the rearmost is inside the rail, so a larger hole has to be drilled in the top of the rail so a screwdriver can pass through for installation. This hole also had the benefit of allowing me to do all the rest of the drilling from above.

With the access hole done, the rails got clecoed back in place and I enlarged each hole first to #30, then to the final size of #21. Then I got to pull it all apart and deburr the holes I’d just made. Remember those forward most holes whose placement I worried about so much? While they didn’t quite land exactly between the two rivets, they’re pretty close, and are nicely in line with the row itself:

This was about the point where I was ready to call it a night. One thing I’d noticed earlier was that all the fitting had scraped up the powder coat on the roll bar base, so I wanted to touch those areas up before installing the side rails for good. So I hit those with the touch-up paint, and then as a last act took a look at those aft most screw holes in the rails. As mentioned before, the screw placement here is further inboard, inside the channel itself. A consequence of this is that the screw head actually interferes with a raised part of the channel, and I’ll have to relieve that a bit so the screw can actually sit flush.

The interference, along with my marks for making the relief, can be seen here:

So that’ll be a good spot to pick up tomorrow (which I happen to have off). I’ll actually need to do one more trial fit, because I forgot one thing: the outboard part of the aft end of the rail actually sticks out past the fuselage sides, and will need to be trimmed. I should have marked that before removing the rails tonight, but I forgot. That’s OK, there were much worse mistakes I could have made.

Once the rails go on for good, there won’t be much left but to start messing with the actual canopy bubble…

Posted in Canopy | Hours Logged: 5

Attaching the center slide rail

OK, it’s time to get back to airplane working again, after a week or so of Other Stuff® going on. Today I decided it was time to grit my teeth, make some holes, and get this center slide rail installed.

Doing this meant first removing the canopy frame and the rail so I could mark a centerline on the turtledeck, which I did by stretching a piece of string between the forward- and aftmost bulkheads. With a few Sharpie marks made, the canopy rail went back in place, as did the frame. The latter was to ensure that I kept the spacing I wanted up in the receptacle area, with the slide block, anchor block, and so forth.

I already had the pilot holes in the rail from before, so I used those to initially drill #30 through the skin, which was easy except for the hole in the forward end of the rail. This sits down inside the receptacle area, and there’s absolutely no space to get a drill in there. That’s probably why the instructions said to drill this hole from the inside, but I couldn’t figure how I’d position it accurately doing that, which is why I drilled the pilot hole.

Getting this hole drilled was fun; I resorted to putting a short threaded bit for the angle drill into the pilot hole, and spinning it by hand – a lot – until I had a decent little pit created in the receptacle floor. With the rail removed, I then (just barely) had enough room to get in there with the angle drill and make the hole.

This brought me to getting the holes to final size for the #6 attach screws. I discovered while doing this that, for some reason, I have a #28 drill bit for this (which is a good snug fit for a #6), but my countersink bit has a #27 pilot. Which means I had absolutely no way of drilling the screw hole and then countersinking it. To solve this problem, I countersunk the holes while they were still #30, using that bit, and only then opened them up to final size. Sorta roundabout, but it got the job done.

Finally it was time to go crawl back in the tail again. With Josie holding the screws from outside, I installed the nuts and washers from inside, and also opened that forward most hole to #28 from inside – which apparently was an operation that needed to be photographed:

After that, I got the frame installed once again, and tested canopy movement. Strangely, the slide block seems to bind up just a little bit – not enough to prevent movement, but it seems to drag a bit. Something to look at later on, I guess.

I’d intended to clamp the side rails in place, but discovered that I’m not entirely sure how to do that. Probably not a difficult problem, but it made a good excuse to call it a night. In the meantime, here’s a look at the installed rail:

Posted in Canopy | Hours Logged: 2

Canopy slide block do-over

This past weekend I found a nice goody in the mailbox – a package from Van’t containing my replacement slide blocks. Yes, that’s “blocks” plural, because I ordered two of them, just in case I messed up a second time. Things have been busy since then but I got some time tonight to give this a second try.

Looking at the first block, I laid the holes out in what was a pretty good spot, but the actual holes ended up a bit lower. So for this attempt, I mostly focused in being more precise with the drilling, but also shifted the hole location up just a hair. As before, I used the center punch to spot the hole locations, but this time, instead of going straight to the drill press, I started the holes with a #40 drill bit I spun with my fingers. This way I could ensure things were starting off lined up. I also put together a spacer of scrap wood to put between the “ears” of the block to prevent the plastic from flexing while I was drilling; this was probably a big part of why the last block got mis-drilled.

From there, I opened the holes up gradually on the drill press; first a #40 bit using the holes I’d already started, then up to #30, and finally #12. That yielded a very snug fit with the pin, so I finished things off by running a #10 bit through both holes just using a hand drill; this gave be a better slip fit for the pin and also ensured both holes were collinear.

The first test fit on the canopy worked great; the anchor pin now sits just a bit above the center rail, and when the frame is slid all the way forward, the pin engages in the anchor block with the slide block fitting nicely between the frame and slide rail. With all that validated, there were some finishing touches to put on the block (or, as I thought about it, a few remaining opportunities to ruin the part).

First, one side of the block needs to be counterbore a bit to allow the clevis pin to sit flush. According to the plans this is required for the assembly to fit in the socket on the fuselage, though from my previous test-fit it worked just fine. But I’m not one to ignore instructions, so I used a 5/16” bit to make a nice little recess, so now the pin sits nice and flush.

The second thing that’s needed is a smaller hole from front to back on the block; this allows a cotter pin to be inserted through the end of the clevis pin and hold it in place. I was a little nervous about this since it required both precisely measuring the distance rom the block edge to the hole in the clevis pin, and also ensuring the hole was vertically aligned with the clevis pin hole. As before, I marked the spot and then started the hole by hand, before drilling all the way through with a #40 bit.

I think this is all that’s needed; there’s no real guidance given here other than “make a hole for the cotter pin.” I think the only thing that bothers me a bit is that the provided cotter pin doesn’t go all the way through the block, so it’s not really secured to my way of thinking. I’m somewhat inclined to look for some longer pins to use here, so they go all the way through the block and the ends can be bent out. Something else to think about…

For now, though, it’s done. Here’s a look at the clevis pin sitting flush, also showing the cotter pin head on the other side. I inserted the pin this way because with the canopy closed, gravity will be helping hold it in, for whatever that’s worth:

Here’s a better view of the cotter pin from the other side. Initially I’d thought of making the hole large enough for the head of the pin – or at least counterboring it like the clevis pin hole – but on second thought that’d make the pin really, really difficult to remove. Keeping the head exposed seems like a better choice to me:

Finally, we can see everything mating together nicely with the frame all the way forward:

Between the slide rail and the anchor block, the rear of the frame is rock solid in this position, though it can still move side to side since the rail isn’t yet secured. But having this done means I’m finally feeling confident about centering up the slide rail and getting it drilled and screwed into the fuselage – and once that’s done, the two forward rails can follow, and then I should be ready to move on to the canopy bubble itself.

Posted in Canopy | Hours Logged: 1.5

Firewall planning

So not a ton to talk about tonight really. Initially I’d figured on threading those CPI2 harnesses back through the firewall and getting the pertinent harness bundles laced for hopefully the final time…but then I got to thinking about whether that was a good idea. The whole reason I had to wait until I pulled the rest of the harness through the firewall is that the engine side of the CPI2 harnesses are already terminated, meaning they have to be threaded through bulkheads from the engine compartment. Thing is, that firewall passthrough may not be the only place I need to thread them. For example, one of the ignition coils will be mounted on top of the engine case, which means that harness will presumably have to pass through the baffles.

Now, that might not be a huge deal down the line – the coil connector plugs can probably be depinned if necessary, I’d just have to identify the connectors and get the right tool. But the crank sensor is a different matter – the wire connections aren’t detachable there. I’m not 100% sure whether or not those wires will need to pass through baffles, but in the end it seemed that the better choice here was to wait on these bundles. I might well end up with a chicken/egg type setup here, though…if I wait until I’m doing the engine baffles, that’ll mean I’ve fitted the cowl, which almost surely would require that the forward upper skin be riveted in…and once that’s done, finishing up the harness bundles will be a lot less fun. But still, I have little to lose by waiting; there’s nothing at stake right now other than me wanting this task done.

So instead I turned to the firewall layout. Some low-hanging fruit here was to go ahead and mount the brake fluid reservoir and cabin heat control box, both of which already have prepunched holes in the firewall. Getting the brake reservoir in place also required riveting a couple nutplates, which I guess were skipped way back when I first did the firewall. The heater box I just clecoed in place for now; it’ll need to be sealed when I final-mount it, and even though that’s still just using a couple bolts, I figure I’ll wait on that.

From that point forward, I was kind of on my own. The one thing that I figured I’d definitely lay out was the manifold block that’ll be used for the fuel and oil pressure sensors. The FWF drawings provided specify a location for that block, and while I don’t necessarily have to abide by that, I see no reason not to. Rather than actually mount it – I’m definitely not ready to commit to anything like that – I just drew an outline of the block and marked the two hose attach locations.

It’s not much, but it’s a start:

The next thing I tried to tinker with was the location of the battery box; since this is a relatively large item and accessibility is a concern, it seems like something to work out early. The FWF plans call for putting it on the right side of the firewall, about halfway up; I’m sure I’ll end up on that side of the firewall, but I’m less enthusiastic about the vertical location. The big question is how to tie the box into the firewall angles; they’re not exactly conveniently located for this. I suspect I’ll probably end up needing to add another angle on the back of the firewall to accommodate this, but the main takeaway is that this requires some thought. Something else to mull over a bit, I suppose.

Of course, somewhere near the end of the night I remember that I could also have been working on stretching the engine mount to better fit the firewall mount holes. Maybe I’ll work on that next; I’m sure I’ll want to install and remove it a few times while working out some of this firewall layout stuff.

Posted in Firewall Forward | Hours Logged: 1.5

Finishing with the engine mount, doing some wire routing

As I headed out into the hangar to get to work this evening, it occurred to me that I hadn’t had a single super bright idea about how to stretch out this engine mount to get the second pair of holes drilled. All that random thinking about making a jig with threaded rod and so forth hadn’t gone anywhere concrete. So I ended up just trying to stare at things and work out a solution, and eventually I got to something.

Basically, there are two ways to approach this: either I need something inside the mount exerting outward force to spread things, or I need something pulling down on the bottom of the mount. The latter seemed impossible since I had nothing to pull against, but finally I realized that if I stopped thinking in terms of using something like a ratchet strap, there were other ways to approach this. What if I could just hang weights off the bottom of the mount and try to work with the positioning that way?

And that’s how I ended up with this amusing Rube Goldberg setup:

We’ve got a 30-pound kettlebell hanging on the center of the mount, using an S-hook normally reserved for hanging up a caliper while working on the car brakes, plus another 30 pounds of dumbbells lashed together with some spare paracord and hung from the corner with more spare paracord. The only real issue with the hanging-weight idea is that you don’t have a lot of fine control over how much the mount stretches, and that’s where the big clamp comes in. Hanging the weights as shown here got the hole just a tiny bit above where it needed to go, so with the clamp in place, I could carefully apply that last bit of force to get it all lined up nicely.

The only remaining issue was how to pull the mount snug against the firewall while doing this; as it sat, the mount face wanted to sit about 1/4” off the firewall. I initially tried using a ratchet strap secured to a long piece of lumber going through the center section, but the strap would have been bearing on the edges of the forward side skins and the firewall flange, and surely would have bent something if I’d started cranking down. Then I had another epiphany – the other lower hole could be used for this. I just had to run a 3/16” bolt through the hole and the mount, add a large washer so it’d bear against the mount hole, and tighten the whole thing down.

That pulled both lower holes up nice and snug, and once I had the lower right hole drilled and bolted, the other was already lined up nicely and didn’t even need any drama to get it set up. The only concern here is how annoying it’ll be to attach this mount unless I permanently stretch it, so I’ll probably have a go at that at some point, but not tonight.

Instead I decided to continue thinking about FWF type stuff. One item I’ve been putting off for a while is drilling the 3/4” hole down the right side of the aircraft for all the engine sensor wires and such to pass through. That seemed like a nice digestible project for tonight, so I got to it. I’d been thinking that laying the hole out properly would be a challenge, but once I got down to it it wasn’t tough at all. The only hiccup I had was that the unibit drifted a bit as I was opening the hole, and got into the edge of one of the firewall angles, so I had to then go in with the dremel and sanding drum to smooth things out.

Once that was done, I installed the snap bushing and had the fun of feeding the wire bundle through from inside, and now I’ve reached the milestone of having random wires sticking out through the firewall:

Assuming I don’t get that replacement canopy block in sometime soon, I think I might start marking up the firewall for component locations, just to sort of spitball ideas. The FWF plans include some suggested layouts that I’ll likely start with, but I’ll have to consider some other items not shown there that I’m adding – like the battery-bus fuse block and E-bus relay. Those are pretty small but they still need homes, and routing of wiring is also a concern.

The other item I could work on now would be feeding the CPI2 FWF harnesses back through the firewall and finishing up the lacing of the relevant harnesses in the cabin. Those had to wait until now, as they’re already terminated no the engine side and so can’t be fed through in the other direction. It’d be kinda nice to finish up those harnesses inside, I suppose. We’ll see.

Posted in Electrical, Firewall Forward | Hours Logged: 2

Fitting the engine mount

Well, I’m still paused on the canopy front until I get in the replacement slide block from last week’s shenanigans, but in then meantime I get to kick off a whole new category with the first bit of firewall forward work. Most of the weekend has been spent working on other stuff around the house, but I wanted to keep making progress on something and so I decided to see about fitting the engine mount to the airplane.

The firewall and the structural bits behind it came with an existing pilot hole at each corner, and I drilled those holes out to 3/16” quite some time ago to allow for the fuselage rotisserie mount. The final bolt holes are 3/8”, but final-drilling those requires some attention, since individual engine mounts can vary even though they’re welded up in a jig.

So the first step is to do a rough evaluation of fit out of the box. To do this, I installed a couple of long AN3 bolts in the upper two holes and used those to loosely hang the mount in place. Doing this allowed me to establish a good starting point, as I could verify that the width of the two upper mount points were at (or very nearly) the same width as the two pilot holes. That meant I didn’t need to do anything dramatic to get those first two holes drilled…well, almost. The construction manual calls for drilling the holes using the engine mount as a guide, which I imagine helps ensure that the holes through the fuselage structure are in line with the actual mount sleeves. So the most interesting part of all of this was figuring out how to “clamp” the mount against the firewall. I probably should have gotten a photo of the final setup, which involved some ratchet straps going from a piece of lumber across the mount to the setback support in the cabin…

In any case, the upper two holes are now drilled and bolted in place. This gives me a nice base to work off of for the other two holes at the bottom: 

However, things down here are a bit less simple; the engine mount holes are a good 3/8” or so above the pilot holes in the firewall. I figured this out by putting flashlights inside the fuselage, pointed at the pilot holes; with that light sources inside, I can easily spot the pilot holes from outside, even if I’m looking through the engine mount itself. Note the pilot hole at the bottom of the engine mount hole, mostly occluded by the mount itself:

So in order to get these drilled, I’m going to need to rig something up to precisely stretch the engine mount. I made a first rough attempt at this tonight, which didn’t work so well. I figured since both lower holes are high, I’d see about trying to push both down, so I flipped one of my large hand clamps to make it into a spreader, and put it between the upper and lower center of the mount. I was able to move the lower holes by maybe 1/4” or so, but still nowhere near into alignment.

I’m not entirely sure yet how I’m going to work this problem, but so far I’ve had some vague ideas involving threaded rods, nut, and bearing blocks, but the hard part would be getting any of that stuff braced in the right place on the mount. Normally I’d prefer pulling for something like this, but I don’t really have anything to pull against…unless I were to put concrete anchors in the floor just for this one operation, and I don’t really want to do that.

So anyway, something to mull over. I’m sure it’s a solvable problem, I’ve just got to work it out.

Posted in Firewall Forward | Hours Logged: 1.5