Static ports in

Super short today. I got myself some epoxy, and then this evening I bonded the static port inserts into place. I thought about starting on my antenna doublers, but decided to just make it a short night.

Static ports from inside:

And outside; here you can see how these ports protrude from the skin a bit, mimicking the profile of the Van’s pop rivet:

That’s it. Tomorrow I suppose I’ll work on the doublers, or else the plumbing to link these two ports together. That’s assuming I don’t feel I need to do some more hurricane prep, depending on what our friend in the Gulf does tomorrow…

Posted in Fuselage | Hours Logged: .5

Paint, static ports, and conduit too!

Nice productive day today, on a variety of stuff, even though I found myself needing things to complete some tasks. First up was getting the remaining bulkhead cleaned and scuffed for priming, then left out to dry while I went across the runway for coffee and chit-chat. By the time I came home, it was good and dry, so I got it primed. An hour or so later, with the primer dry to the touch, I went ahead and shot the stone texture coat, which I then left to bake in the sun. Apparently the heat and sun really help this stuff cure – previously I’ve found this paint to still be smearable a day later, but this time it was dry to the touch by mid-afternoon. It was actually dry enough that I went ahead and clecoed it in place in the fuselage, though I’m still going to wait until probably next weekend before doing any riveting, just to be sure.

Hey look, paint!

So with nothing more to do on the bulkheads, I needed a new task, and I decided to get going on the static ports. This ended up being a prime example of how vulnerable I can be to “analysis paralysis.” Before doing anything, I went inside to just look at some static system install photos, and ended up reading a whole lot of discussions about issues with static ports.

To preface this conversation, the plans method for static ports is, in the great tradition of Van’s, dirt simple – you just remove the stem from a pop rivet and bond it into a hole, then stick a tube on the inside portion. This is a touch crude for me (and others), so some time ago I bought a kit from SafeAir1 that included machined static port inserts.

Thing is, some people have reported airspeed issues with the SafeAir1 ports. From further reading, I learned that the first kits sold placed the static ports flush with the fuselage skin, unlike the pop-rivet method, which would put the ports slightly proud of the skin. Fortunately, later kits remedied this and left the ports similarly proud, and this is the type of port insert I have. Of course, there were still people reporting airspeed issues with those ports as well. Some people went so far as to install the port inserts on the outside of the skin, but still other people opined that this might cause errors due to being too proud of the skin.

Long story short, I could have spent all day trying to figure out the exact right way to do static ports, but in the end I was able to just go and install the ones I had. It seems that if I end up having any issues, they can be addressed a few different ways, so in the end I just did the thing.

Van’s says to place the ports four inches below the longeron rivet row, and one inch forward of the adjacent bulkhead row. Since the flanges on these inserts are larger than the plans pop rivets, I moved the hole an additional quarter-inch forward, to ensure clearance with the bulkhead flanges. After measuring a few times for good measure, I drilled the 1/4” holes, one on each side of the tail.

then there was the question of how to mount these. Some people rivet them, one people bond them, some people who really like to combine belts and suspenders do both…I decided I was just going to bond them. If it’s good enough for my fresh-air scoop forward, it’s good enough for this. So I scuffed up the mating surface of the inserts, as well as the mating area inside the skins:

Here, though, I hot a roadblock: I don’t have any epoxy on hand. So much for bonding these today. I actually considered going out to buy some, but that seemed like an unproductive choice, especially since I’d probably have to go into Katy to find anything. Instead, tomorrow I can just run into Brookshire when the hardware store is open.

OK, so what next? I know, I can finally install the conduit that took me three tries to buy, and work on the pitot tube heat wiring. First up was locating the conduit holes; I reviewed the Van’s guidance on placement, which OKs a location between the forward most lightening hole and the adjacent one. I picked a center location that provided good distance between the rib edge, the lightening hole, and the stiffening ridge between the holes. I was initially going to make some sort of a jig so I could locate all the holes in the same place, but had a better idea, just using the intersection of an arc drawn off the hole, and a straight line off the rib edge.

With the holes located, I drilled pilot holes and then busted out the Unibit to open them up to 3/4”:

Then I measured the conduit run (about 24”), cut off some conduit with extra length for good measure, and pulled it through the holes. I see some people report having a lot of trouble doing this when they use this for wing wiring, but I found it pretty simple to pull through. The key is to stretch it was you pull, making the outside diameter shrink a bit so it goes through the hole more easily. I pulled the conduit relatively snug between the ribs so it wouldn’t sag, which should make running wires easier. Finally, I applied RTV around the conduit on each side of the rib penetration, to stabilize it in place and prevent vibration from cutting the conduit:

All right! Next I’ll locate the pitot controller and drill its mounting holes…wait, that’s a bad idea. I’ve got wet RTV down there, probably not a good plan to do drilling above that and embed aluminum chips in the RTV. OK, we’ll move on to wiring instead.

Since I’m extending the wiring between the controller and the tube, I’ll be adding an extra pair of terminals, which will need to pass cleanly through the conduit. This is particularly important, since my plan for dealing with the service loop of wire and pitot line will be to pull the slack out to the wingtip and secure it there (as opposed to letting it just sit loose in the wing bay).

Problem is, as supplied, the terminals both on the controller and tubs sit right beside each other, which would make for a very bulky spot in a snug conduit:

So I basically re-terminaled both the controller and pitot harnesses, staggering the wire lengths, which will allow the whole bundle to be slimmer. Once it’s assembled, I expect to wrap both joints in silicone tape or something just to help smooth them out even more. Here’s the same harness from above after trimming:

OK, now the RTV is pretty dry, so let’s get that controller located. To make this a little easier, I transferred the shape of the controller base into thin scrap plywood and thus made a template. I used the template to locate the first mounting hole, checked the actual controller in place with that hole, then used the controller itself as the template fo the other three holes. I considered going ahead and putting in the nutplates here, but for the moment I think it’s actually easier to use clecoes to temporarily mount the thing. Here it is with the two wiring runs roughed up: the feeds from the wing root coming out the white PEX conduit, and the harness going to the pitot tube going into the black ribbed conduit:

Finally, I had everything in place where I could make the extension harness that will go through the conduit! Well, actually not, it turns out. I only have red and black wire in the gauge needed for this run. Black isn’t an issue, since that’s the actual color of one run, but the other two are blue and orange. I’m not OCD enough to need the colors to actually match for those, but I do want to use an acceptable generic color, which is white. Red implies a power run – which these are, in a way, but I don’t like the ambiguity. I’d rather match the wires on the pitot tube harness, where there’s one black wire, and two white ones with heat shrink color-coded to match the controller wires.

So yeah, I need to order some wire to make this extension harness. And I guess colored heat shrink as well, but that I already found on Amazon, so that’s easy. Not sure where I want to order the wire from, I think I’ll be figuring that out tonight.

Hopefully tomorrow I can get those static port inserts bonded; if so, then I can go ahead and get the static line routing in place between the two ports. Just one more little thing.

I’ve also been thinking about my other conduit runs in the fuselage. I think I’m going to want two runs under the seat floors: the right side can house the wiring harness going to the aft avionics bay and tail, and the left one can route the pitot and AOA lines back to the ADAHRS. The other fun thing is the conduit I’d intended to run in the tail; if I run it through the holes I originally planned, it’ll exit into he baggage area, which I don’t want. Instead I think I’ll end up with a curved run, starting low in the bell crank area and ending up high at the tail. The challenge here is that the conduit run will go around a longeron, and I’ll need some way to keep that contact from wearing through the conduit over time. I’m not actually sure that this idea will work…another thing to think about…

Posted in Electrical, Fuselage, Wings | Hours Logged: 3.5

Bulkheads!

Just a bunch of bulkhead work today. I’m kind of wishing I’d gotten a head start on this one of the previous two nights, but oh well. Originally I was thinking I’d be able to get these all riveted in place in the next work session, but I forgot one crucial step: the forward most bulkhead needs to be primed and painted before it can go in, since it will be visible in the interior. And before that can happen, some subassembly needs to be done.

I started off today picking up with deburring all the stuff I’d match-drilled previously, then moved on to the various dimpling and countersinking operations. Basically, I prepped every part except for the actual skin, which I’ll handle when it’s time for it to go on the airplane. There’s plenty of holes to mess with here, so this did take some time.

Next up was some assembly. The harness fairleads and canopy rail receptacle got riveted in place. The former was straightforward, as was the latter…kind of. An issue here are the three lower rivet holes, whose shop heads sit inside an acute angle. There’d definitely be no squeezing those with the tight clearance, and even bucking them with my skinny tungsten bar would have been a challenge. So I decided to use blind rivets on these instead. But then I was bothered by the idea of having some the rivets here be solid and the others blind (since the heads will be visible), and so I ended up just using blind rivets for all nine holes. Oh, and I had to drill out and replace two of them, because they didn’t quite go in perfectly flush.

It was late in the day by this point (I spent the middle of the day going out for pre-hurricane supplies), so priming today was out of the question. But hey, while I couldn’t rivet that one bulkhead, the other three could go. So I took those over to the fuselage and got them riveted. I was a little concerned about this, since some of the rivets joining the upper and lower bulkheads sit kind of tight against the skin and/or longerons, but I got them all squeezed with no trouble. Oddly enough, the most problematic ones were on the aft most bulkhead, which rivets to the aft deck. The two outboard riveted there are super close to the longerons, and I tried about three different ways before I ended up shooting them with a long straight set.

So now I’m all – well, mostly, I guess – bulkheaded up:

Hopefully tomorrow the rain holds off and I can get the last bulkhead primed and painted. It’ll still be a bit before I can rivet it after that – I’ve found previous that this granite-texture paint can take some time to really harden, so I’ll want to let that part sit for probably a week before I abuse it by doing some riveting. Kind of thinking I might go ahead and install the static ports and the first part of the plumbing while I’m in a bulkhead-ey mood. Maybe finally get back to the wing wiring stuff too, now that I have my conduit.

Posted in Fuselage | Hours Logged: 3

Fitting the aft top skin

Boy, it’s been a while since I did a good old-fashioned cleco-match drill-uncleco work session. Kind of nice to do something so mindless, actually…

With the prep work on the harness anchors complete, tonight was just match-drilling the aft top skin to the bulkheads and other components. First, though, I had to knock a few years’ worth of collected dust and spiderwebs off the skin. If I’d followed the construction manual to the T, I’d have gone ahead and removed the blue vinyl and deburred the skin edges, but I figure I’ll leave the vinyl on until I’m about ready to put the skin on for good. For now, I just want to get to the point of riveting the upper bulkheads in place.

Anyway, with the skin cleaned off a bit, on it went. Getting it clecoed was a little interesting, particularly aligning the two center bulkheads, where I can’t just take one hand and move it into alignment. A straight pick was useful for inserting into one nearly-aligned hole, and then maneuvering the bulkhead so an adjacent cleco could go in. Then it was just a bunch of match-drilling.

Look ma, a turtledeck!

And then it all came back apart again… Look ma, no more turtledeck!

Next I get to do a bunch of deburring, plus figuring out what parts of the manual to do now vs. save for later when the skin goes on for good. I suppose the reasonable thing would be to just get deburring and dimpling done on the bulkheads and maybe the other parts that go in assembly. I’m thinking I can probably get these bulkheads riveted in place in my next work session.

Posted in Fuselage | Hours Logged: 1.5

Harness anchor prep

Not a lot to look at tonight – I just did the prep/modification work on the rear seat shoulder harness anchors. Last time I mentioned the idea of using shims between the anchors and the skin in lieu of filing a relief for the bulkhead flange, and…I decided not to do that. When considering the shim idea, I had a sort of vague thought that what I was considering might weaken the joint’s shear strength, but I couldn’t quite put it into words. As I figured might happen, someone on VAF set me straight.

Basically, simply adding the shim into the joint would result in it effectively “floating” between the anchor and the skin. Obviously this wouldn’t involve lots of movement, but in a case where the harness was put to the test, the shim could allow for a tiny bit of relative movement between the anchor and skin, thus allowing the rivet to stretch and/or bend a bit, instead of acting in pure shear.

There’s no telling how much this might compromise the joint – it might be tiny for all I know – but in the end, I don’t think it’s worth it to go off-plans here. So today after work, I got to filing. To make things easier, I clamped a 2×4 block in the vise and match-drilled a few holes using an anchor as a guide, which let me cleco the anchor in place while I worked on it. Next, a block of 1×4 scrap wood, clamped in place against the closest flecks, acted as a guide for the filing. All I had to do was keep the side of the file along the block as I worked, to get a fairly straight cut:

After a fair amount of trial and error, the relief was looking good. However, I didn’t want to leave the sharp edge left by the file and block, so I next went to the bench grinder and removed material to make the transition more of a bevel:

And finally, I did some fairly aggressive radiating of the long edges that will sit against the skin. The reasoning here is that these flat pieces will be attaching to a curved skin; I expect the radius should help these more easily fit snugly against the skin:

After this, it was time to go get the grass mowed, followed by dinner. I guess next up I get to cleco the skin in place and do a bunch of match-drilling…

Posted in Fuselage | Hours Logged: 1

Just a bit more fuselage stuff

Today I was soundly beaten by the Houston heat. I got some work done in the morning before going across the runway for coffee, but after that I just wasn’t up for dealing with it.

During that single hour, I deburred the canopy receptacle and got it clecoed in place and match-drilled. Then I ended up doing some trimming on the gussets I put in place yesterday. They didn’t fit well against the bend radius of the bulkhead, and the wouldn’t sit flush, so I had to remove some material from the corners.

The next step would be to get the actual skin deburred and put in place, which can maybe be a task for tomorrow. A more pressing thing I’m thinking about is the two shoulder harness anchors. These are riveted to the top skin and the second bulkhead back from the rear seat, and are made out of thick alclad sheet. What’s interesting is that they need to sit flush against the skin, but also need to be relieved for the additional thickness of the bulkhead flanges.

By the plans, you’re supposed to file this area down to fit, but that seems like an unpleasant way to deal with this. First of all, this fitting has to be done with the skin in place, which means working inside the tailcone, which is already not fun. It’d be even less fun with the trial-and-error that comes with fitting work like this.

So I’m entertaining a different option – rather than filing the anchors down to allow for the bulkhead, why not instead make shims out of .032” sheet (same thickness as the bulkhead) to go between the anchors and the top skin? This seems like it’d achieve the same goal of ensuring the anchors sit flush, without the filing and trial-and-error. The only issue I can think of is that the additional material might make the joint a bit less strong in shear, which would be the expected loading if the harness was ever asked to do its job.

I’ve asked this question on the Van’s forums; it’ll be interesting to see what kind of responses I get. There are some good engineering types in there that ought to be able to point out any horrible flaws in this plane.

It also occurs to me that I could possibly do the filing of the anchors (per plans) without the repeated fitting if I use my .032” stock as a guide, which makes it a little less unpleasant. It still puts the onus on me to do some very precise removal of material, though.

Anyway, that’s it for today. It remains to be seen how much I get done this week, as it’s supposed to stay hot about all week. At least I’m still getting small things done from time to time…

Posted in Fuselage | Hours Logged: 1

Fuselage bulkheads

So I find myself working with a new sort of challenge when it comes to productivity on this project: namely, the fact that there ought to be plenty of things to work on right now, but I keep having trouble actually doing stuff. I’m fixating on the tasks that I really want to be doing – for example, the pitot heat plumbing that I’ve been trying to get the right conduit for. Granted, the August heat here in Houston also isn’t especially motivating, but still…

Anyway, as of yesterday my order from Van’s still hadn’t come in. Also included in that order was some 0.040 sheet stock, which I’ll be using to fabricate doublers for my antennas, and which I’ll want on hand before drilling the mount holes for those. That’s both the thing I’ve been trying to do put on hold. I was hoping the Van’s stuff would be at the post office today, but I wanted something to work on this morning.

What I settled on were the upper bulkheads in the tail, which will support the aft upper skin. I was originally going to leave these until I was ready for that skin, but while looking at running conduit back to the tail, I saw that the predrilled conduit holes go through the overlap between the lower and upper bulkheads. Ergo, if I wanted to get that conduit installed for running the wiring back there, I was going to need the bulkheads permanently installed first. And hey, the bulkheads aren’t the access problem, the skin is…might as well get going.

So I first spent about two hours deburring these things. Lots of nooks and crannies tom give attention to, lots of time with a needle file. This is often tedious, but today it felt good to be doing something (and I don’t just mean sweating). Next up were the harness fairleads – these reinforce the slots in the forward most bulkhead where the harness shoulder straps will pass through. These are thick aluminum stock and thus need some vixen file attention before going to the scotchbrite wheel. To be honest, I’m still not super satisfied with the smoothness, especially inside the slots. I think I’ll end up doing some more work on those with sandpaper or something.

Next, the fairleads were clecoed into place and the rivet holes match-drilled, then all the bulkheads got checked in place to the fuselage, and the rivet holes joining them to the lower bulkheads were match-drilled as well. The last thing I did before calling it a (sweaty) night was to add the gussets behind the forward bulkhead. Presumably these are to keep these from distorting, since they’ll potentially have a passenger leaning back against them. Only the bulkhead has prepunched holes for the gusset, and not the longeron – I guess I’ll get to drill those in assembly at some point. Interestingly, as I read forward in the instructions, it never actually says to do that, as far as I can see…

Anyway, here’s the fuselage with upper bulkheads in place:

Next up I get to add the canopy rail receptacle (at the top of the forward bulkhead) – this is what the aft end of the canopy will drop into when closed. Then I get to add the aft upper skin and other stuff and do a bunch of match drilling. At this point I’m thinking that I’ll get all the fitment tasks for the upper skin done, so I’m just short of riveting it, then I can put it aside until that time comes. Between that and other minor stuff, I should be able to keep busy until the end of the month, when I expect to – gasp – place my avionics order.

I got a quote from SteinAir this week, and I think it’s about time. All the mockup work I’ve done with cardboard cutouts of avionics boxes is all well and good, but I want the real things in place before I start actually making shelves and figuring out wire runs. I just can’t get comfortable with doing that stuff based only on cutouts, regardless of how correct they might be.

Posted in Fuselage | Hours Logged: 3

Conduit comedy

Apologies for the amusing alliteration in the title…but it’s an appropriate summary of my feelings today, and maybe a small lesson in just following the plans, so to speak.

Recall that I went shopping for conduit sometime last week, so I could add a short run from the wingtip to the pitot tube location. Now, this isn’t uncharted territory, since Van’s provided solid instructions for running this ribbed conduit through the wings, and even sells the conduit themselves. But they also only sell 25’ of it at minimum, and I needed maybe ten total, for the wing run plus some runs int hen fuselage. So I ordered what I thought was the right size from Amazon, but it was too large – I’d clearly mixed up the inside vs outside diameter dimension. But now I knew the thickness of the conduit, so I couldn’t go wrong. I ordered the right size, and now surely I’d be in business, right?

Well, I picked the package up from the post office (along with another package…more on that in a bit), and came home ready to finally Do Something®. Except…this time the conduit is too small. And there’s no intermediate size for sale on Amazon. Now, this isn’t an immediate deal-breaker – since I’ll be making my own holes in the wing ribs for that run, I can use whatever size I want. But some tinkering revealed that the 1/2” stuff I got in today is too small for even my short wing conduit run, since it needs to accommodate terminals alongside two pitot lines.

So yeah…here we are, a week or so after the odyssey started, and I have a couple lengths of conduit that I can’t really use, and I’m about to just order the stuff from Van’s anyway. If only I’d done that in the first place…

But hey, let’s talk some more positive stuff. As I mentioned, I had another package – this was from Don Pansier of Delta Pop Aviation, containing the antennas I ordered late last week. It’s fun getting stuff like this, starts to really feel like I’m turning this aluminum hulk into a functional aircraft:

 There was one unexpected aspect of this order, though. When I placed the order, I went with two com antennas, one 1090MHz transponder antenna, and one 978MHz/UAT antenna. The former is for, well, the transponder, and the latter is for the ADS-B receiver. So I was a little surprised when I opened the box and saw that both the blade antennas appeared to be identical. This, by the way, is the reason they’re still in their bubble wrap bags in the photo above – I thought maybe I’d gotten shipped the wrong things. I wrote Don a quick email to ask about this, and he responded (at 8 PM) to explain that the antennas were identical, and would perform equally well, and included performance documentation. I’ve heard stories of Don’s great customer service, and he didn’t disappoint.

Finally, after the conduit shenanigans, I did want to get something constructive done tonight, trivial as it might be…so I went with getting the autopilot roll servo mount kit installed. This is pretty simple – you just replace the lower bellcrank pivot bracket with the supplied piece, and add a support arm off the upper pivot bracket. To get that support arm properly positioned, I put the servo I have on hand in place temporarily, and went ahead and assembled the linkage from the servo to the bellcrank just for good measure:

Once again…moving from spare parts too systems. Fun stuff to play with, even briefly. But that’s it for tonight…I think now I need to do some research into antenna positioning, then I can see about getting those mount holes located and drilled. I figure the main thing will be making sure the com antenna locations are moved aft a bit so they can’t interfere with the aileron push tubes, and I’ll want to space the blade antennas a bit off of adjacent structure to allow for good access as well.

And maybe I’ll finally get the right conduit I need this week…here’s hoping if I order tonight it’ll be here Friday…

Posted in Wings | Hours Logged: 1

Fuselage teardown

Welp, this was one of those days where you kind of step backwards in order to move forward, or something similarly zen. I did get the conduit ordered from Amazon, and it did go out for delivery today, but via USPS, and they held it at the office, which means I won’t have it in my hands until Monday at the earliest. I may actually wait until Tuesday, as I also have my antennas coming – I ordered those from Delta Pop Aviation Thursday evening, and they’re already on their way.

So with that in mind, I decided it was time to bite the bullet and get serious about the fuselage. Which meant removing most of the assorted stuff I’d put in there over the past several months. The tail feathers came off and went back into storage, the roll bar and panel came out, all my cardboard avionics mockups got put away, the control column and elevator pushrods got put by the wayside…and now it’s back to just looking like a canoe:

I also vacuumed out everything, which basically means I sucked up a whole ton of dead june bugs. Then I got the fuselage back into the rotisserie, and rolled on its side so I could look at the belly. Since the antennas are coming, I figure I’ll go ahead and get their mounting holes done once I have the templates in hand.

But first, I had to figure out where to put the antennas. There are four that I need to find homes for on the belly: two com radio antennas, and two blade antennas, one for the transponder and one for the ADS-B receiver. There are assorted placement requirements that kind of dictate where these will go. Specifically, the ADS-B receiver antenna needs to be at least 2’ from the transponder antenna, and the transponder antenna wants to be at least 3’ from any com antenna.

The com antennas should optimally be separated by 6’, but that’s simply impossible on an RV-8. Most small aircraft handle this by putting one on the belly and one up top, but there’s nowhere up top to do this. So the accepted thing for about every RV-8 I’ve seen is to put the com antennas just behind the main spar carry through, each one as far outboard as possible.

That means the other two get to go further back, and this is a segue into another consideration for placement: I want to be able to access these antennas relatively easily from inside the aircraft. That is, I don’t want them to live under any panel that’s riveted in place. The com antennas satisfy this, since they’ll be under the removable forward seat floor/footwell area. Further back, I have the rear seat floors and the forward baggage floor to consider; both of these will be riveted in.

This leaves two usable regions: the first is basically under and ahead of the rear seat, around where the rear stick is located. The other is aft of the baggage floor. Given the separation requirements, the most sensible thing seems to be to put one antenna in each region, and since the most confining requirement is the separation between the transponder and com antennas, that pretty much says that the transponder is going in the aft location.

So with all that in mind, I made rough marks on the belly as to the location of each antenna. These will of course need to be refined before I can actually drill holes; I need to figure out how far outboard the com antennas can go, make sure they won’t interfere with the aileron push tubes, and similarly check for interference for the blade antennas. But this setup gives me a little over two feet between the two com antennas, a little under two feet between the com antennas and the ADS-B, a good 3.5’ between the ADS-B and transponder, and over five feet between the coms and the transponder.

Works for me.

 

So that’s it for today. I still need to put away a lot of the stuff I removed today, and then maybe I should review the riveting instructions for the forward bottom skin – that’s been deferred for way too long.

Posted in Fuselage | Hours Logged: 3.5

Just organizing stuff

Not putting any hours on this since I don’t consider it active aircraft work, but over the past few weeks I’ve been accumulating a lot of small stuff – connectors and associated stuff to go with my electrical junk, and then today a pile of cushion clamps and snap bushings from Aircraft Spruce. Most of this stuff has been sitting out on tables since it came in.

So I went to Harbor Freight a couple days ago and once again increased my inventory of storage boxes, then just started unpacking and storing stuff tonight. Now, among other things, I have a case full of connectors and terminals and a whole bunch of D-sub backshells:

Some less-great news: the conduit I ordered from Amazon, which was intended to be used to route the pitot controller wiring extension, is way bigger than I anticipated. I guess I was thinking that the conduit diameter specified was the OD, when in fact it’s the ID. So this stuff is kinda huge. And so now I need to order some more. Maybe if I get the order in tonight it’ll come Saturday, it’s like that pitot extension thing is my white-whale task or something.

On the other hand, I also got my AP roll servo mount kit, so I can get that installed on the right wing. I am really thinking the next big thing to do is get the tail feathers back off the fuselage. I think I keep putting it off because it looks so much more like an airplane with them on there…

Posted in Workspace