Updated antenna positions

I had previously planned the antenna positions both disconsidering convenience of mounting the antennas, and assuming I'd have the MotoPOD on the bottom. Given this, I took some time to re-plan their placement taking both into consideration (click on any of these for a larger version - original file here). In these drawings, the solid circles are the ideal ground planes, and other circles are additional restrictions.

Top view - ELT, Stormscope, COM, GPS and TAS antennas
I no longer need separate UAT and transponder antennas. Given that Garmin requires a minimum of 3' of cable from the transponder to the antenna, I moved that antenna to the rear part of the tailcone:

Side view with all antennas

Bottom view - transponder, COM, NAV and TAS antennas

I added a third GPS antenna - one for the GTN, one GPS+XM for the G3X (PFD only), and one for the G5.

TAS antenna details - ideal and minimum ground plane plus distance to other antennas
I moved the bottom TAS antenna to inside the forward tunnel, since the aft part of the tunnel has no easy way to run cables to it, and very little clearance near the skin, with the elevator pushrod going through it. The distance between the top and bottom antennas is about 21", which should add a bearing error of about 0.2˚ for a target at 1 mile (perfectly acceptable, I doubt the TAS has that level of precision anyway):

Distance between the two TAS antennas - this introduces ~0.2˚ bearing error for a 9 or 3 o'clock target at 1sm

With the transponder antenna moved aft, I'll try using the original XPDR antenna hole for my bottom COM antenna. It's unclear what kind of performance I can get from the ground plane at that location, but since the ground plane area is only about 20% smaller than the top antenna's, I'll just plot the VSWR after the tailcone is attached and see (and if that doesn't work, I'll add another hole in the baggage area and plug this one).

COM ground plane area is ~1371sqin (ideal is ~1662sqin, ~20% more)
I was also briefly worried that the tailcone antennas might be too close to the ground in a maximum takeoff rotation position, but a quick measurement showed that's not the case (i.e. the tail would hit the ground first):

Tailcone antenna ground clearance at maximum rotation attitude

Given that none of these require any structural changes for now (only the top TAS antenna will give me trouble), I'm deferring any installation steps to later when I actually have the avionics - who knows what else may change until then.

Mid-fuselage ribs and bottom skin deburring and dimpling

The outboard rear seat ribs weren't aligning with the skin holes, so I had to flute them, which was quite annoying when already attached (I even got a smaller fluting plier just for this):

Fluted outboard rear seat rib
I match-drilled them properly and removed the skin, then started deburring and dimpling all the ribs and bulkheads for

Deburred and dimpled ribs
All center section bulkhead holes and the holes with tabs on other bulkheads were machine-countersunk:

Machine-countersunk holes on aft center section bulkhead

Dimpled and machine-countersunk holes on rear spar bulkhead

Dimpled and machine-countersunk holes on fuselage bulkhead
Next I need to deburr and prime the skins so I can start riveting them on.

Time lapse:


Total mid-fuselage ribs and bottom skins rivets: 412
Total mid-fuselage ribs and bottom skins time: 75.0h

Forward-fuselage bulkheads and bottom skin progress



Forward + aft portions of the fuselage attached together for drilling

I measured the wing spar at exactly 1.7" thick. When I first attached the center spars with spacers, I instead measured it at close to 1.8":

Spacers measured around 1.8" (should be 1.7")
Turns out that the thickness of the blue vynil adds up quickly, and 28 layers of it per set of spacers wasn't helping. I removed it and deburred the parts for some extra smooth coupling:

Spacers with all the blue vinyl removed
That got me almost all the way there (about .02" to go):

Spacers much closer to 1.7"
Since the spacers were slightly curved, I just applied force to make them flat. I could have torqued the nuts, but I don't have a torque wrench that can do the required 1100in-lbs (will order one for when I need to attach these semi-permanently until the wings are actually attached), so I instead just squeezed them with clamps - first with my usual plastic clamps, which did pretty much nothing:

First attempt at compressing spacers, using regular clamps
Then I used the heavy-duty clamps with some felt padding (idea credit goes to the wife):

Successfully compressed spacers with heavy-duty clamps
and with that, holes were magically aligned :) so I final-drilled all of those, and started deburring some of them.

Time lapse:


Total forward-fuselage bulkheads, ribs and bottom skins rivets: 0
Total forward-fuselage bulkheads, ribs and bottom skins time: 44.4h

Firewall riveting mostly complete

I modified my #30 dimple die using the grinder, to dimple the bottom-most holes in the firewall bulkhead:

Modified dimple die for dimpling the bottom holes of the firewall bulkhead
then continued riveting:

Fully-riveted firewall forward side

Fully-riveted firewall aft side

With this, the only parts missing on the firewall are sealant (which I plan to apply later) and the rudder pedal brace (which I didn't want to install until I figure out how it'll work with the ControlApproach pedals).

Time lapse:


Total firewall rivets: 596
Total firewall time: 58.4h

Mid-fuselage ribs riveting done, skins started

We finished riveting fuselage bulkhead and baggage ribs:

All mid-fuselage ribs and bulkhead riveted in place

I clecoed the bottom skins on and final-drilled all the holes:

Mid-fuselage section with skins on
The floor stiffeners required some fluting to line up properly, then they were final-drilled as well:


Floor stiffeners, fluted and final-drilled in place

Mid-fuselage section with skins and floor stiffeners only (it barely clears the ceiling!)
I found that the holes from the skin to the outboard seat ribs don't align :( so I'll need to flute that part, which will be especially tricky with it already riveted in place:


Since I only have a vise-grip-style fluting plier, which would be even harder to use in this space, I've ordered a regular plier from Spruce and will give that a try when it gets here - I have plenty of other holes and edges to deburr in the meantime.

Time lapse:


Total mid-fuselage ribs and bottom skins rivets: 412
Total mid-fuselage ribs and bottom skins time: 67.5h

Mid-fuselage ribs riveting, part 2

With the parts all primed, I started by riveting various small parts to the ribs:

Step mounting brackets and seat rib subassemblies riveted together
Of course, while doing this, I realized that two little parts had been forgotten when doing primer :( so one more primer session had to be done:

Two seat belt attach lugs I forgot to prime :(
I got lazy this time and decided to do it with rattle-can primer. The color difference doesn't really matter since any apparent parts of the interior will be painted anyway:

Rattle-can-primed seat belt attach lugs, riveted to the rib
I also inserted the heat tee, which allows me to continue riveting the ribs:

Rear tunnel with heat tee installed
I riveted some of those ribs so far:

Most rear seat ribs have been riveted in place

Time lapse:



Total mid-fuselage ribs and bottom skins rivets: 326
Total mid-fuselage ribs and bottom skins time: 55.2h

Firewall riveting

I dimpled then started riveting the firewall parts by the forward seat ribs (aka tunnel), adding all the nutplates, the inspection panel backing plate, the fuel valve attack bracket flanges, and the scat tube support:

Inspection panel backing plate/cover, fuel valve flanges and scat tube support with nutplates riveted

Forward fuselage ribs with nutplates, inspection panel backing plate, nose gear tension fittings and fuel valve bracket flanges riveted on

Forward fuselage rib riveted to nose gear tension fitting

I then dimpled the recess box and the firewall bulkhead to accept the rivets:

Dimpled firewall bulkhead
and finally started riveting it all together:

Firewall bulkhead with most parts riveted to it

Forward side of the firewall bulkhead, with most parts riveted to it

In the process, I also realized that the rivet gauges I have don't match Van's spec - Van's allows smaller shop heads overall, and with some of the rivet lengths they specified, it's impossible to get to the gauge's "official" spec. This applies to most firewall bulkhead rivets, so I had to measure those with a caliper - specifically, the gauge has a hole that's about .19", and the spec calls for .163". The height was almost right on the gauge - the gauge has .06", and the spec is .05".

"Standard" rivet gauges don't really match the MIL-spec that Van's recommends

There's still quite a bit of riveting left to do, but this is a good start.

Time lapse:


Total firewall rivets: 512
Total firewall time: 49.9h

Started fuselage side skins

I got started on the dreaded section 29 - Fuselage Side Skins.


Longerons and roll construction angles ready for cutting

The first part of this is bending of the longerons, which is a lot of brute force with a mallet to get them to match the template:

Longeron matching template after bending

Time lapse:


Total fuselage side skins time: 6.4h

Mid-fuselage ribs and firewall primer

We finally did another batch of primer, after periods of heavy smoke, then business travel, then too-cold weather. This included parts from the mid-fuselage bulkheads/ribs and the firewall:

Some parts drying after washing with PreKote

All parts after PreKote

Ribs, firewall and inspection panel parts after primer

Ribs and firewall parts after primer

Ribs, firewall, ventilation ducts and inspection panel parts after primer

Ribs and firewall parts after primer

A less-than-amused primer applicator at the end of the day
With this, we can finally resume riveting for both sections!

Time lapse:



Total mid-fuselage ribs time: 48h
Total firewall time: 24.4h

Forward fuselage countersinking and inspection panel

I finished machine-countersinking forward-fuselage parts:

Machine-countersunk center section side plates

Machine-countersunk fuel valve flange brackets

I then continued to installing the tunnel inspection panel - this starts by drilling the rivet holes onto the tunnel rib:

Tunnel inspection panel rivet holes match-drilled

then marking and cutting the rib for the panel:

Tunnel rib with corners of panel opening drilled out

Cutting edges of the tunnel rib panel opening

Tunnel rib panel opening
After that I trimmed the hole slightly to make sure the cover plate fit nicely over the doubler:

Tunnel rib with backing plate clecoed on

Tunnel rib panel with cover plate on

I also got some work done on some parts that are officially done as part of section 28, but not used/installed until later for some reason:

Seat floor assemblies drilled, deburred and machine-countersunk.

Mid seat rail supports drilled, deburred and machine-countersunk
With this, most of these parts are ready for primer.

Time lapse:


Total forward fuselage bulkheads and ribs time: 34.5h

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