I started out today by applying orange Torque Seal to all the gear mounting bolts in the hell hole.

I then mounted a 1×2 vertically on the firewall, offset 3/8″ so that I could then mount a horizontal 3/4″ wide board down the CL of the fuselage.  I originally was going to use my German aluminum long boards for the alignment board, but it wasn’t as straight as the 1×4 pine board I had on hand.

Here’s a shot of the 1×4 CL alignment board.  As you can see, completing Chapter 13, the nose gear, allowed me to set the nose gear at just the right height & use it as a mount. Pretty darn handy!

I set & verified the CL alignment board with a plumb bob at a few spots along the length of the board.

Here’s a shot of the installed CL alignment board.

I then clamped my own version of the “Straight Tower of Pisa,” somewhat like my buddy Marco did.

A shot of the left axle clamped in place, with a square attached.to it.

Another selfie for the FAA, right before I started in on all the major sanding of the gear bow.

I sanded the left gear leg down to set the toe-in.

Then, when I started checking the toe-in on the right gear, my measurement at the gear strut came out right about 0.12″ farther outboard than the left side.  I strung up my plumb bob over the center mark on the gear bow & confirmed that the gear was set about 0.12″ off center to the right.  Not sure how this happened since I had it dialed in while in Germany, but it was definitely an issue that I felt I should deal with.

After some thought, I decided to simply add 6 plies of BID on the exterior side of the left gear to move the wheel out about 0.1″.  Really, I don’t think being an 1/8″ off would cause any noticeable issues, but I want to keep the wheels difference from CL under 0.07″ or smaller.

After getting the initial toe-in set for the axles, I sanded down the entire gear legs for both the axle mounting BID gear pads, and the eventual installing of the gear fairing.

Here’s a shot of the right gear leg after final sanding.

I then double-checked the lower gear leg markings . . .

. . . and then initially trimmed the end of the gear legs.

Here’s another shot of the trimmed gear legs.

Here’s the specialized gear trimming tool . . .  ok, it’s a jig saw!

I then test fitted the wheel assembly onto the end of the gear leg.

Another shot of the wheel assembly test fit.  I still have some lower gear glass to trim, but this is a good start.

Here’s a wide angle shot of the whole axle install effort.

I cut the 3″x 3″ square BID plies for mounting the axles.  I cut 2 sets of 3 plies of BID for the right side, and then 1 set of 3 plies and another set of 9 plies for the left side.

I then prepregged the BID pads in sets of 3 plies,

and wetted them out.

I then laid up the BID onto the lower gear legs.

Lower gear legs 3-plies BID (outboard right side)

Lower gear legs 3-plies BID (inboard right side)

Lower gear legs 9-plies BID (outboard left side)

Ok, I then let the epoxy cure for over an hour to set up to just tacky before mounting the axles to minimize the slipperiness & sloppiness of the wet BID. Well, it didn’t make any difference really.

To be honest, I’ve never been more pissed off during this build than this step right here.  If ever I should have followed my buddy Marco’s lead & taken a page out of his book and pre-drilled the axle bolt mounting holes it is here.  Trying to mount multiple components to a surface with multiple curves on BOTH sides with clamps is, to put it politely, stupid at best.  Hats off to other builders that have done it, but as I said it was truly the most infuriating thing I’ve tried to do on this build.  It also may be that the Matco axle base is narrower than the other brands, not sure, but it was about impossible (at least for me) to keep so many variables in check.

With the nearly cured glassed getting tweaked by the constant re-clamping of the axles, I eventually chucked them and simply used the face of the heat shields to determine toe-in. For any builders reading this, I would highly recommend this route.  That combined with just laying up the BID one side of the gear leg at a time to minimize variables and slop.

I say this because after the sheer ass-pain with the left gear, then of course I spent well under 10 minutes on the right gear side mounting the heat shield and back axle plate.

As for the toe-in figures, my goal was to keep the difference between the 0″ measurement and the 24″ measurement between 0.1″ and 0.15″ to ensure that there is some toe-in, but not too much.  I hate to say it, but this is one of those layups that I’m crossing my fingers and hoping on, since it looked good after I was done clamping it all together, and 10-15 minutes later… but it’s late, I’m turning it and who knows what will greet me in the morning.

Tomorrow, I plan on pulling off the tape backed heat shields that are certainly in the slightly wrong position, finalize the clean up the bottom gear leg profile, and then mount the axles & wheels.

I started today by doing some more research and analysis on the steps to install the axles to the main gear legs.  It’s interesting because just about every builder I know installed the axles and determined the toe-in angle close to the method described in the original plans, but to a builder they all did something significantly different than the way the plans detail the process.

Although I’m not casting doubt on the plans method entirely, I do want to optimize the process for installing the axles to the main gear & also in dialing in the toe-in angle, so some non-plans steps are most likely in order.  Admittedly, since I haven’t finalized the final flow of how the axle install process, I’ll knock out all the prerequisite steps and let the process reveal itself (said while sitting in meditation position . . . ha!).

In the shop I started by spending about 45 minutes filing the edges of the heat shields to finalize their shape and remove any heinous, finger-shredding burrs (see heat shields below).

I then determined the position of the left axle on the gear strut that allowed for the optimized placement of the brake caliper to minimize the removal of the bottom gear strut material.

After setting the angle & position of the axle on the left side, I made up a template using tracing paper.  I then transferred the mirrored image of the left side axle placement onto the right lower gear leg.  Once I finalized and confirmed the placement of the axle on the right gear leg, I then made up a template for the right side as well.

These will be used IF I decide to follow the plans method which says to sand down the lower outboard gear leg to dial in the toe-in angle before trimming the gear leg or mounting the axle.  Clearly if I sand the lower gear leg, all my markings that I just finalized will be wiped out.  Thus, with my templates I can reapply my markings after shaping the gear legs for the toe-in.

Here’s the right side lower gear with both the axle placement and lower gear removal markings shown.

Once I finalized the positioning of the axle, I used the wheel mounting flange as a template to drill the 1/4″ mounting holes in the left heat shield.

Here’s the left heat shield mounting bolt holes drilled with the test fitting AN4 bolts installed.

And here’s the right heat shield mounting holes drilled.

A shot of both heat shields with the holes deburred & the sides filed smooth.

After finishing with the heat shields, I started work to attach the aluminum squares to the axles to determine wheel toe-in.  I wrapped the axles with tape to protect them from any out of control glue gunk.  I also used a zip tie to keep the square tight against the axle.

I then used the free square to ensure that the first square I was gluing to the axle was …. yep, square.

I then glued the second square to the other axle.

Tomorrow I’ll borrow a page out my buddy Marco’s book and build a smaller version of his “Straight Tower of Pisa” to track the fuselage CL and dial in the toe-ins for each wheel assembly.  After I get the tower built, I’ll start the steps to mount the axles to the gear legs.

I started off today doing some final research on the threaded axle caps (p/n VA-106) from VANs Aircraft that makes installing Sam James’ wheel pants to Matco wheel assemblies doable without having to drill & tap the end of the Matco axles.  After speaking with the guys at VANs & confirming that I had the correct part, I ordered a set.

Down in the shop I started by torquing the main gear mounting bolts (AN6-80A) to 275 in/lb as outlined in CP 46.  For added strength I also added a couple drops of red Locktite to each bolt.

I then spent over an hour leveling the fuselage and ensuring it was square & plumb.  As I started this process, the fuselage was really off as I tried to level it from side to side.  I finally did some investigating and looked inside the overturned fuselage.  It was then that I realized that the fuselage had slipped off on one side of the 2×6 sized board that I had it resting upon.  Once I corrected that little SNAFU, it made the process of leveling the fuselage much easier.

In addition to shimmying the fuselage to get it level, I also used the threaded rod leveling feet that I had mounted in each corner of the fuselage dolly for the first time.  They’re a bit narrow in diameter, but they definitely help.

Here’s another shot.

Once I ensured that the fuselage was level, I measured the distance between the main gear legs and points on the forward gear strut & the forward nose centerline.

I took 3 measurements from each gear leg, then shot 6 measurements to each leg from 2 different forward points on the nose & nose gear leg, respectively.  In the end, I had 9 measurements for each leg, 3 for each specific point.  I averaged each set of 3 numbers, determined the delta between the left & right gear for each set of numbers, then averaged those final deltas to get a final averaged aggregate delta.

When I originally mounted the gear I had determined that one side of the main gear was a 1/4″ farther aft than the other.  However, I was using a standard measuring tape when I originally mounted the gear.  When I used the laser measuring device this time, my delta between the left & right side gear legs came out to only 0.087″, which is fantastic as far as I’m concerned.

After I determined that the gear legs were a close match in both elevation (I checked when I leveled the fuselage by placing a long level across the gear leg bottom edges) and forward & aft, I then determined the WL of the center of the axles.

Since the longerons sit at WL 23.0, and the axle centers are at WL -22.0, then it stands to reason that by simply measuring 45 inches from the top of the longerons to the lower gear legs that I could determine the axle mounting location.  Now, there does need to be an adjustment as Marco points out on his blog since LPC#45 moves the 3/8″ bolt holes on the main landing gear mount extrusions up 0.4″, which isn’t accounted for in the WL -22.0 dimension.  Thus, this moving the bolt holes up 0.4″ makes the new height of the gear at WL -21.6.

So when I measured the height of the center of the gear axle, I subtracted the 0.4″ to make the dimension 44.6″ up from the longeron (when the fuselage is upside down) to the center of the gear axle location.

Here’s a shot of the approximate center point of the axle at 44.6″ below the longeron (at WL -21.6).

When I marked the left side gear leg, the 44.6″ mark was 1.3″ away from the end of the center of the gear leg.  I really wanted another 0.2″ inches, and then lo & behold I realized that the other side of the level pressed against the longerons had slipped a bit.  Once I wedged the level back tight against the longerons, I remeasured the left side and was able to reclaim my 0.2″ so that the 44.6″ mark was at 1.5″ above the bottom of the gear leg (below with the gear upside down).

I wanted the 1.5″ gap between the bottom of the gear leg and the center point of the axle since the axle bases, as shown below, are 2″ square.  Since a half inch provides room to remove some of the lower gear leg for clearance for the Matco brake calipers.

Here’s the 1/2″ mark on the left gear leg.

Below are the Matco axles clamped into place to test the fit, both on the left & right gear leg.

In preparation for mounting the axles to the gear legs, I made a run to Home Depot today and picked up some aluminum squares and a plumb bob, as you can see in the pic below.

I then went back to work on the main gear wheels.  The first thing I needed to do was torque all the bolts to ~99 in/lbs (8.5 ft/lbs).

I then disassembled the brake assemblies in order to isolate the brake disk mounting flange that I will need to mount the wheel assemblies onto the axles.

I first removed the 2 longer bolts from the outside edges of the calipers.

I then removed the 4 large diameter bolts in the center of the caliper assembly, and laid out all the parts as a sort of inventory & acquaintance of the parts, but specifically to ensure the brake pads looked ok & weren’t cracked (which happened to my buddy Marco).

Tomorrow I plan to mount a few 2x4s to the fuselage dolly as a quick frame to help assist in measuring the toe-in for each wheel.  I’ll also be determining and aligning the wheel assemblies to the fuselage centerline.  Within the next few days I plan on having the wheel assemblies installed on the lower gear legs.

Today I got the tire & tube mounted to the other  wheel.  Since I was trying to get at least this one thing completed for the build before I headed out to dinner, I didn’t balance the yellow stripe on the wheels, so I guess that will somehow either make the plane fly crooked or the wheels not in synch!  Although I try not to sweat the small stuff or be too anal as to add unneeded time to the build, had I noted the position of the yellow stripe, I would have mounted the tires symmetrically.

Just like the previous wheel I inflated newly mounted tire to 50 PSI.  I’ll watch the tire pressures for about a week and make sure they sustain 50 PSI, and when I’m sure that they’re are no leaks, I’ll inflate both tires to 70 PSI.

Here they are, my officially mounted tires!  Again, I’m running Lamb 11 x 4.00-5 tires on Matco W50LT wheels.

I then added the brake assemblies to the wheels for these pics.  I’ll still have to torque the bolts to the appropriate specs as I do final mounts on each of the wheel components, so the only actual torque job on my immediate list is the main wheel halves.

Finally, here’s a couple shots showing the width & depth of the brake assembly mounted to the inboard of each wheel.

Again, tomorrow is Superbowl Sunday so although there will be a fair amount of tours of my EZ-building shop, I highly doubt if I’ll get any work done on the plane.

Due to prepping for a Superbowl Party that I’ll be having at the house on Sunday, I didn’t get any work done on the plane yesterday.

Today I mounted the extended firewall to the aft fuselage early on in the day.

Here’s a shot showing approximately what the new profile of the aft fuselage will be when the plane is finished.  Of course this is upside down, but clearly the width & bulk of the fuselage will be extended aft to create more of a “boat” shape vs. the traditional swoop of the old P-51 style inlet.  In short, my Long-EZ will have the same profile as one that has a NACA scoop intake.

That being said, I will have a 3″ round air scoop, somewhat like James Redmon has on his Berkut 13, that will run from aft of the landing brake and slowly meld into the bottom hell hole area so that it should (still in design phase) dive aft into the firewall and flow into the lower cowling skin.  Thus, I guess my EZ will look a tad different than all the NACA-scooped EZs.

I had pulled the main landing gear bow out a few days ago, but just this evening –with the help of my buddy Greg– I sanded down the gear legs for the eventual adding of the gear fairings, and then (re)mounted the main landing gear bow back onto the fuselage.

Although there was the usual fight to get the bolts in, I was pleased that in the end, after a few years of the gear being off & redoing the washers on the mount extrusions, that the gear fit back into the mounts with only a little bit of banging with the hammer required.

Here’s a vertical shot of the main gear legs.

I thought I’d add this pic to show you all what the battery strap for securing the main battery in place will look like.  This is an initial sample that strapworks.com sent me to finalize the custom strap that I’m having them make for me.

Tomorrow will be a light build day since my buddy Greg is over & tonight will be a late night drinking beer & swapping war stories in front of the Chimenia on the deck.  In addition, I’ll be doing the final preps for the Superbowl Party, which of course will consume all of Sunday.  I did receive my tire inner tubes so I plan to mount the tire & tube onto the other wheel.  Finally, I bought some lumber for creating a frame around the gear legs to allow me to position the wheels on the gear legs, align the wheels to each other and to dial in the toe-in correctly.  I’ll get the lumber unloaded & situated in the garage so I can start in hot & heavy on Monday installing the axles onto the gear legs.

I got a late start today so I didn’t get nearly as much done as I wanted to tonight.

I started out today by removing the peel ply from the main landing gear bolt swap foam insert layups.

I figured at some point I should add a selfie for the FAA, so here it is!

After cleaning up the aft fuselage landing gear bolt layups I then marked up the lower firewall to cut for adding the extension.

I then marked the lower firewall to cut the matching “puzzle piece” interfaces with the wood extension piece.

After cutting the “puzzle piece” notches in the lower firewall, I then test fitted the firewall extension.

I then floxed the firewall extension piece to the lower firewall & glassed with 1 ply of BID.

And peel plied the lower firewall extension addition.

After glassing the firewall extension I then traced the gear leg brake disk heat shield template onto the 0.09″ thick 6061 Aluminum plate for cutting.  Again, I’m using 6061 Aluminum as a heat shield since it’s much more corrosive resistant than 2024 aluminum, and in this application, strength is not really required.

I then cut out the heat shields using my jig saw.

I then test fitted the axle mounting flanges on the heat shields.  So far, so good!

I pulled the gear out tonight to clean it up & then mount it, but then I realized that I needed to sand the entire gear bow in preparation for attaching & glassing the gear fairing to it.  It was too late to undertake a big sanding job, so I’ll do it tomorrow.  I also plan to drill & tap a hole on each axle end so that the axles are prepped for the eventual mounting of the wheel pants.

I started off today by removing the clamps from the upper gear mount bolt foam covers that I micro’d & clamped into place last night.

Here’s a shot of the right side upper gear bolt foam inserts micro’d in place.

I then used the Stanley Surform “cheese grater” to knock down the excess foam.

Again, right side after “cheese grating.”

I then did something that I rarely do on this build: I grabbed some of the ton of excess urethane foam I have on hand and cut blocks to fill in the lower bolt holes.  Honestly, with as little foam as there is at the lower edge of the bottom longerons, I could have probably just as easily floxed the existing corners & called it a day.  But since this edge will have more foam added to it to fill in the space for the aft fuselage fill-in/lowering to match the 4″ lower firewall & cowling, I went ahead & filled these bolt troughs with foam.

Right side lower bolt troughs filled with urethane foam.

I then micro’d the urethane foam filler pieces into place in the lower gear bolt troughs along the lower aft fuselage edge.

I then used 2 tape-covered pieces of wood to cover the freshly micro’d in place urethane foam inserts and clamped those across the aft fuselage (hellhole).  Here’s the left side fuselage.

Since I had one extra small piece of foam all by itself on the lower right side I needed to give it a little extra attention, so it got its own clamp (bottom of pic).

And a wide angle shot of the clamped urethane foam inserts.

While the micro cured I went to work on cutting the firewall extension piece.

I pulled out the box containing my 6mm (1/4″) Finnish Birtch plywood.  The plywood box being easily spotted… recognize it?  It’s the box that I primed all the 2024 aluminum extrusions for the wings & CS spar.  Ah, memories!

Anyway, I pulled out the second uncut 24″ x 48″ sheet that I still have left over from my original order of 2 sheets, but then found the remaining piece left over from when I cut the original firewall.  This piece was plenty big enough from which to cut the 4″ firewall extension.

I marked 4″ up from the bottom edge of the scrap Birch plywood sheet, and then placed my existing firewall in place with the vertical edge aligned flush with new plywood edge & the firewall bottom edge aligned with the 4″ line on the plywood.

I then traced the bottom of the firewall in relation to the marked 4″ line across the plywood piece, and then again along the very bottom edge of the plywood piece.  The latter will be the new bottom edge of the firewall.  I then made 3 puzzle piece styled locking tabs to help lock the new 4″ firewall extension in place when it is attached to the bottom of the existing firewall.

Here’s a closeup of the “puzzle piece” tabs.  I grabbed a 27/64″ (.421″) drill bit and traced the bottom edge of it to the side of each puzzle piece tab to mark the drill points that will make up the compound curve of each locking tab side.

I then drilled a smaller pilot hole for each circle I just marked.

Loaded up the mojamma 27/64″ bit . . .

. . .  and drilled the holes to make up the compound curved edges of the puzzle piece locking tabs.

I then used my jig saw to cut out the rest of the 4″ lower firewall extension piece.  I would have preferred to have a finer jig saw bit, but since it will all get covered with glass anyway, I wasn’t too concerned about a slightly rougher edge.

Here’s the new firewall extension piece mocked up along the lower edge of the existing firewall.

In the pic below you can see the paper template that I will finish tweaking in order to cut out the 0.09″ thick 6061 aluminum heat shields for the lower gear legs (as per CPs).  I’m using 6061 vs 2024 since it is more corrosion resistant, and that will be a definite benefit in the lower gear & wheel well environment.

Here’s the lower gear heat shield test fitted onto the wheel brake assembly.

After all my ancillary shenanigans above, the micro on the lower urethane foam inserts was at least 80-90% cured, so I proceeded with the final glassing of all the foam plugs covering the main gear mount extrusion bolt heads.

I sanded down the urethane foam inserts to match the contour of the lower fuselage edge.  I have to say that I haven’t worked with urethane much, and it is definitely SOFT, so it requires a much more delicate touch than I admittedly used in sanding the inserts to shape.

After locating & cutting my scrap BID pieces to cover the foam inserts, I then micro’d all the foam pieces.

I prepregged 6 pieces of 1-ply BID, laid them up over the foam inserts & then peel plied all the freshly laid up glass.

This completes the main landing gear mount extrusion bolt washer swap!  Although it essentially added 3 days to the build, the piece of mind it provides is well worth it.  I’m very happy that I did the swap and also very pleased with how it turned out.

Tomorrow I’ll be working a lot various components in prep for the gear install: cutting the bottom of the existing firewall & floxing/glassing the 4″ extension to it; cutting out the heat shields from the 0.09″ aluminum sheet; leveling & truing the fuselage; cleaning up the gear bow in prep for mounting; shaping the inboard wheel pant support bracket, etc.

I started out today by making some noise!  I was able to quickly get the 1/4″ mounting bolts out of the left side of the aft fuselage, leaving some rather securely embedded washers in the process.  I tried to quickly remove the washers but they weren’t budging, so I left them for a bit while I removed the right-side bolts.

All was going well until I got to literally the last bolt to remove.  I have to say I’ve always been impressed with the size & strength of the aircraft grade MS21042-4 nuts, but one huge disadvantage is that if you make one good slip up with the wrench on a very tightly installed bolt, and POW! . . . It’s stripped!  And that’s exactly what happened with this last nut/bolt that is one of two –including the other side– that are pretty difficult to reach.

Well, I messed around with this *!&$#@ nut for almost half an hour to no avail.  I pulled out the whole armada of tools that I have in the shop … again, with no avail.  Thus, in my overwhelming need & desire to win out over an inanimate object (and believe you me, this sucker was INANIMATE!) I figured since I had loosened it up even by the slightest degree, that it had to come out.  But, just about as far down on the inboard side in a “V” channel as you can get, there was just no way to forcibly remove the nut & pound the bolt out.  I was going to have to attack it from the accessible outboard side.

I taped up the inside of the upper bolt trough with aluminum foil tape (I took a pic but it turned out really blurry) to protect the foam from the sparks.  As you can see below, I missed a spot.  Nothing like the smell of burnt foam in the morning to wake you up!  I spent a good 5 minutes with the Dremel grinding off the bolt head, and then another 15 minutes getting the remainder of the bolt, with nut attached, removed.

As I was using a center punch from the outboard side to dislodge the jacked-up bolt, I quickly realized that it wasn’t going without a fight.  If it was departing the airframe, then it was going to bring the lower forward landing gear mount extrusion with it.  I don’t know why, but this bolt was seemingly fused to the gear mount extrusion bracket.  I eventually let it have its way by unbolting the 2 top bolts to get the whole extrusion bracket out of there.  Now, this was after creating about a 1″ gap between the interior side wall (15-ply BID pad mounting base) and the outboard mounting surface side of the extrusion.  With this gap, I snuck in my small German hack saw and cut the bolt in half… another solid 5 minutes down the drain!  Once the bolt was cut in two, I drove the whole assembly back towards the side wall to get enough clearance to free up the bolt that at this point was gouged & stuck into the aft side of the GIB setback (you can see the divot in the pic below).

I then removed the gear mounting bracket with the remainder of the Bastard Bolt from Hell! still stuck in the bolt hole.  Even after all this, it still took some really sharp blows with the center punch to get this damned bolt removed from the bracket!

Here’s the skeletal remains of the Bastard Bolt from Hell! after I dismembered it!

Thankfully, it took only about a minute to remove all the scorched foam & clean up the bolt trough.

And here are some more casualties of war.  I’m still not sure why I mixed up the AN960-416L washers for the standard ones, but again, that completely solidifies my decision to spend a few days swapping out these main landing gear mount attachment washers.

Back to the “peaceful” side of the fuselage, I spent a few minutes (I should add the words “longer than needed” here!) removing the embedded washers.  To keep with the slog of a day that I was apparently mired in (ha!) I bent the tip of scribe trying to get these damn embedded washers out!  I finally resorted to using a 1/4″ diameter cylindrical punch pin to insert into each washer just enough where I could then push the pin to one side and pry out the washers.

I employed my new found trick on the right fuselage side and removed the washers handily.  I then embedded Saran wrap in the aft holes in prep for flox, but in the forward holes I wrapped the Saran wrap with electrical tape to have a dark identifying marker for the bolt hole since I would have to drill the forward bolt holes from the outboard side with no mounting bracket holes as a guide.

This wasn’t just on the right side where I had the issue with the stuck bolt, it was simply a matter of access to drill the holes on the inboard side of the fuselage.  The upper mounting bolt holes on the forward main gear mount extrusion simply are located higher than the aft lines of the GIB seat back.  Unless I was using a flexible drill bit attachment, it was physically impossible to get access to the inboard side bolt holes to drill them.  Thus the dark protective plastic in the forward upper bolt holes.

I then grabbed a couple of strips of the scrap BID that were left over from the nose layup I did a couple of weeks ago.  From the BID I made up 2-ply BID pads to prepreg & layup in the upper bolt access troughs cut into the side of the fuselage. I also added a 1-ply piece of BID to repair the punctured seat back from when I removed the Bastard Bolt from Hell!

Below are the left & right shots of the laid up 2-ply BID pads over flox to reset the “floor” of each bolt trough back to level after the damage of the original bolt heads & washers getting embedded too deep in the surface.  As I’ve stated before, this damage was part & parcel to having the bolts installed with enough clamping pressure to keep the landing gear mount extrusions mounted securely.  Yet another reason I’m really pleased to be performing this washer swap.

While the flox & glass was curing I went to work to knock out some ancillary tasks.

First, I grabbed some spare 3/4″ thick Divinycell PVC foam & cut them into blocks to match the dimensions I had measured earlier for each of the upper mounting bolt troughs cut into the side of the fuselage.  As you can see, they’re identified with the letter designator that I labeled each bolt trough with.

I’m not exactly sure how I’ll deal with the lower gear mounting bolt troughs that I opened to expose the bolt heads along the very bottom longeron edge of the fuselage.  I’m not really that concerned about the aesthetics of these lower bolt-access troughs because they will reside directly under the newly mounted fuselage sidewall lower extension foam that I will be adding to fill in the aft fuselage to account for a 4″ lower firewall.  Again, this is to match my Carbon Fiber engine cowlings that were designed by Mike Melvill & fabricated by Feather Light.

With the upper bolt hole foam inserts cut to size, I then started on installing the tires & tubes to the Matco main gear wheels.

And here’s the end result.  One wheel with the tire & tube installed, and yet another casualty!  On try #1 I followed Matco’s directions by adding about 10 PSI of air into the tube when it was installed in the wheel before bolting both halves of the wheel assembly back together.  This made the process nearly impossible, even with clamping both halves together.

So, round #2 I followed the sage advice of Frank Sinatra and, “Did it my way!” by not adding any air, clamping the tire down to ensure that none of the tube would get pinched, then bolted it together and filled ‘er up to about 50 PSI (70 PSI is max on this tire/tube combo).  Voila!  It worked!

Note that each time I did use talcum/baby powder to reduce the friction of tube going into tire.

Also, I will order a couple more tubes from ACS later this evening.

After messing around with tube & tires, I spent a couple of hours making a few phone calls before returning back down to the shop.  The flox & BID in the bolt troughs were nearly completely cured, so I pulled the peel ply . . .

. . .  and then re-drilled the bolt mounting holes.  I have to say that I’m glad I used the dark plastic material for the inserts since I could see where to drill the holes on the forward bolt holes.

After trimming the upper aft AN970-4 washers to fit, I then vacuumed out the troughs & then mixed up some wet flox using fast hardener.  I spread a good bead of wet flox on the forward gear mount extrusion and installed it.

I then started on the forward extrusion after mounting the bracket back into place, and mounted all the remaining bolts & washers after applying wet flox to inside face of the AN970-4 washers.

Here’s a shot of the bolts & new large washers installed with wet flox on the left side of the fuselage.

After I ensured ALL the main landing gear mount extrusion bolts were torqued to 70 in./lbs I notched the inside of the trough foam inserts to fit over the bolt heads, whipped up some thick micro, and micro’d them into place in the troughs.  After determining the fit was good, I clamped the foam inserts into place on each side of the fuselage.

Here’s a shot of the aft end of the fuselage (Hell hole area) showing the foam insert clamps in place.

I have to say that after mounting the bolts I was even more convinced that I had made the right decision to swap out the washers simply by the fact that the remaining threads on each installed bolt went from about 8-10 remaining previously, to around 2-4 threads visible after the washer swap.

Tomorrow I’ll be looking to finalize the installation of the large washers by embedding new foam inserts into the lower bolt troughs, sanding down all the foam inserts and then laying up the final glass to cover over the foam replacement inserts.  I’ll also be marking up another piece of Finnish Birch plywood for the 4″ extension to the bottom side of the firewall.  I’ll also most likely pull out the main landing gear bow to clean it up & prep it for install onto the fuselage.