Rough River 2017 – Bits ‘n Pieces!

My first interest poking around the various birds at RR17 was how other builders had configured their nose hatch release latch.  I took special note of Rick Hall’s freshly built Cozy IV setup.

Here’s Rick’s homemade latch catch:

I then noted James Redmon’s nose hatch release.  His is from McMaster-Carr.

As is the other Berkut that was there that James helped build extensively.

Simple latch catch on the Berkuts.

Again, here’s the other Berkut:

The Berkut’s also had this spring loaded button that provided the small force necessary to pop the hatch open.

Here’s another nose hatch release.  I also noted a myriad of folks placing their GPS pucks on top of their batteries… hmmm, interesting use of space.

Speaking of space utilization, Terry Sherman followed Davenport’s design and added some baggage space flooring in the nose to keep the baggage from gumming up the rudder pedals.

I then had a number of discussions on aileron fences.  Seems like everyone who has them, including James Redmon, really tout the positive impact they have on the flight controls.

Here’s some more.  Again, seems like these might be a good trick to try.

While discussing engine baffles with Buly (more on this in upcoming posts), he noted that I should ensure to place a steel cross brace between the alternator and starter.

I then noted some differences between many styles of baffles used in canards.  Buly recommended that instead of making my own baffles, I order a kit from VANs.  One advantage to the VANs baffle kit is that it exposes the alternator & starter so that they’re easily inspectable during preflight.

Terry Sherman has a cord plug to easily hook up and warm his engine.  Good thinking…

Terry also has a one-way suction valve much like race cars do to vent his crankcase right into the exhaust pipe.  I’m interested in this and will assess it much further.

I noted on Rick Hall’s Cozy that he had a cork plug in the center of his Silver Bullet prop hub: Nice simple idea for keeping moisture out of the prop’s wood core.

With the help of a world-renowned hand model (Bruce Sinclair…ha!), I was able to accentuate this pic of James Redmon’s removable nose avionics area cover [attached to the canard on the Berkut].

Steve Beert pointed out that the Cozy IV’s have a removable nose avionics area cover just aft of, and NOT included as part of the canard cover (as the Berkut’s is).

The Cozy IVs use a hinge pin system as seen on many standard tractor aircraft cowlings.  The pics below show both the left and right side hinge pin assemblies.

Back to James’ Berkut 13, I really appreciate the simple way he uses his outboard wing-to-winglet fairing to pin his rudder gust lock into place.  Very nice.

I then took note of some winglet configurations and N-number styles.

This looks like a robust way to secure the right side canopy if need be:

And a very cheap, lightweight, and simple solution for a canopy push/pull handle.

Here’s a cheap mirror that James Redmon attached to his canopy to see what’s going on behind him.  He has one on the other side as well (I guess you could say it’s “a mirror image!”  . . .  yuk, yuk!)

And a nice cheap & movable method to keep sunlight at bay.

I also grabbed a shot of how James used a RAM mount for the GIB headrest.  I like this since it would easily collapse if need be.

The Berkut has some nice features in its design such as these water runoffs that actually vent through a hole out onto the strake surface.

Since I’ve been working on my heating & fresh air ventilation system, I was interested in James’ pilot fresh air vent, which many other builders have copied of course.  James painted his cover black…

Where the other Berkut owner just used the interior paint to cover up the plate.  Both look great so I wanted to capture a shot of each.

I had a nice discussion with James on his pilot fresh air intake scoop since he changed it from the original tear drop shaped inlet on the bottom side of the strake, just aft of where the new style (seen below) is now.  James states the new style produces so much volume of fresh air that he had to make a restrictor for the inside of it, whereas the old teardrop style produced almost no fresh air and he could barely feel any flow with his hand pressed against the vent.

I took this shot for the paint colors, winglet configuration and N-number style.

Not surprisingly, I see a lot of canard aircraft with some rather unseemly ways to tell exactly how much fuel is showing in their fuel site gages (read: ugly!).  I really appreciate how clean and simple James depicts the amount of fuel in his fuel site gages (could very well be white on black labels from a label-maker, but still very clean and legible).

As before, I really liked the simplicity and style of this paint job.

Also, the wheel paints were blended in nicely with the gear leg.

As were the gear legs to the fuselage…. nice work both on finishing and paint on this Long-EZ!

I also grabbed a few shots of James Redmon’s RAM air belly scoop since I’ll be doing very close to the same thing for my RAM air scoop.

Alas, then it was time to go home.  But nothing beats FLYING back home in a LONG-EZ!  Thanks Marco!

When Marco & I returned back to Chesapeake Airport, we had some time to kill waiting for Gina to come pick us up. So we meandered over to some other builders’ hangars to stop them from working for a while! <grin>

One of Marco’s EAA buddies, Dale, is working on an RV-9.  He showed me his VANs baffling kit and highly recommended using it.  He also showed me how he routed his SS lines for the manifold pressure and oil pressure sensors.

I also took note of how he ran his upper ignition wires through a hard grommet in the baffle wall.

One of my biggest surprises was Dale’s instrument panel.  It looked awesome and was the charcoal gray color I was looking for (vs matte black).  He said it was simply a 3M vinyl product that he discovered other folks using and he got it off of Amazon.  I’ve already pulled the trigger on some and can’t wait to test it out!

Before I left, as I was helping Marco work some stuff on his bird, I quickly took some measurements to use as a reference in the upcoming months when I construct the top of my nose.

Out of curiosity, I also measured the distance between his NG30 and interior nose sidewall.

So that’s the last of what I have as far as our Rough River 2017 trip… hopefully these visual notes helped you in figuring out a thing or two as they did me!

 

 

Rough River 2017!

As I mentioned in my last post prior to Rough River, I’ve been on the road ever since.  I’m still hanging out with friends in North Carolina and will be for about another week. Nonetheless, I wanted to get some RR 2017 pics posted.  Unlike the usual plethora of airplane pics however, these are a bit more personal (read: people pics).

The first pic was one Marco shot while we were waiting for the fuel dude at Central Kentucky Regional airport.  We were chatting in front of the fuel pump when Marco noticed the reflection of his bird in my glasses, so he quickly took this pic.  As I’ve noted to a number of people that have been saying they don’t recognize me due to my full beard, the fullness of it is merely a result of me trying to pour as much energy as I can into the plane build… and not worry about “needless” things that waste time…. like shaving!  haha!

This was the first night’s dinner at a local pizza joint where Marco grabbed an opportunistic selfie of all of us…. note Marco in the lower left corner, Steve Beert upper left corner, then Mike Beasley, Bruce Sinclair and me (with my hand over my mouth, in shock over something “Potty Mouth Bruce” had just said! ha!).

A bit later we had a few libations in our cabin… this pic was taken right before Nick Ugolini and Buly Alevant showed up.

Here’s a shot of the next day, when Mike, Bruce and I were checking out Bill James’ Vari-Eze.  John Lambert was walking around snapping pics, and shot the next few pics of us hanging around Bill’s Vari.

A shot of the gang with Bill James.

Understandably, Marco spent a fair amount of time fielding questions regarding his new instrument panel upgrade, which left me, Mike Beasley and Bruce Sinclair to fend for ourselves!

Here’s Marco’s new panel that he upgraded from traditional steam gauges.  He installed two GRT Mini-APs as his PFD & MFD, and a Garmin GNS480 WAAS GPS unit. His Mini-APs have the capability to drive GRT AP servos, which he’ll be installing next.  He did a great job on this panel, and just in time for Rough River too!  (You can follow his panel upgrade adventures here).

When Marco took a breather from extolling the virtues of his GRT-based panel, we checked out Nate Mullins’ Long-EZ  (cracks me up whenever I think about it, since for years Marco continuously stated that GRT would be his LAST choice . . . until he saw my Mini-X come to life on the bench! ha!)

All good things must come to an end, so Sunday morning found us on our 3+ hour trek back to home base (Chesapeake, VA).

Ah, mission complete!

I’m so grateful to have such an awesome friend like Marco, and to have great adventures as his GIB.  But I have to say this RR really reinforced my passion for finishing my Long-EZ so next year I can relinquish Marco’s back seat to its rightful owner: his wife Gina!

Good times!

Cheers.

 

Chapter 24 – Pilot seat floor glassed!

This will be my last build post prior to Rough River!  And since I’ll be on the road visiting folks in North Carolina and Virginia, I won’t be home for another 2 weeks…. so quite the break in build action.

Today I pulled off the boards that I had clamped in place to help straighten out a rather wavy looking foam piece that I shaped into a curve for the pilot seat floor piece, which also happens to make up the majority of the pilot thigh support.

I then cleaned up the initial Kevlar layup and test fitted the floor seat piece without the boards in place.  It looks good, but still needs just a bit more persuasion to be close to spot on.

I also rounded the aft edge into a radius that I assessed as a “pleasing shape” since I plan on doing all glass to glass edges on this seat floor piece.

I then did the round #2 top seat floor layups on both the front and aft side of the piece, overlapping onto the initial Kevlar layup.  The duct tape squares you see in these pics that you might be curious about are 2 pieces of 1.1″ x 1.1″ duct tape plies covered by another 2 plies of just slightly wider duct tape.  These duct tape pads are to provide clearance on the underside of the seat floor piece for the 2 ends of the EFII fuel pump frame that juts aft. The foam over these 2 tape pads, and of course the tape itself, will be removed before I layup the underside of the seat floor.

So, at the outset of the round 2 layups, I set a square of peel ply over each of the duct tape pads and then laid up a 2″ x 2″ ply of reinforcement BID over each of the pads.  I then laid up the separate front side single plies of glass (1 BID & 1 CF) to reach aft enough to cover the tape pads.

Once I got the layups completed and peel plied, I then set the seat floor back in place and clamped it again to try and knock out some of the waviness incurred by heating it up in the curve-shaping process.

You may note that I used some carbon fiber over on the left side.  This is due to the fact that I had some scraps of carbon fiber hanging around, and I also wanted to really lock in that corner and tame an indention over on that side.

A few hours later, when the glass was about 90% cured, I removed the clamps and checked out the layups . . . all good!  Moreover, the slight indention on the left side was in fact tamed and is no longer an issue.

I then pulled the peel ply and cleaned up the layups.  Here’s a test fit of the pilot seat floor after round 2 of the top side layups.

Then it was on to round 3.  I micro slurried what little bare foam was left, and made some transitions (as I had on round 2) with thicker micro between the edges of the Kevlar and the foam.  I also filled in the divot created in the upper right hand corner where the clamp piece of wood made a distinct edge.  I actually liked the depression, but glassing it could have been a bit difficult, so I simply filled it in with dry micro.

I then glassed the second and final ply of BID on the seat floor top.  For some reason I felt like going rogue again and did NOT peel ply the entire layup, just the inside edge that will have a mini wall glassed in around the fuel selector valve.

A few hours later, after the final BID layup on the top of the seat floor cured, I then razor trimmed and cleaned up the edges, and set it back in place for a test fit.  So far I’m really happy with how this is turning out.  To be clear, it’s not perfect, but definitely good enough for this combat builder!

With the top done I got on with the task of shaping the front edges and sides of the underside of the foam seat floor.  Just like the top aft edge, these 3 sides will have a radius that will allow the glass to curve around the edge in one continuous piece to make up the edges of the plate.  Thus, every side of this seat floor plate will have micro’d corners for strength.  This obviously mandated that I had to spend a bit of time making the angled trenches along literally every exterior edge (minus the center U-shaped notch) of the seat floor plate.

I then spent a bit of time as well pulling the tape & peel ply out of the divots I created for the fuel pump frame jut-outs that I needed clearance for.  Once all the remnants of the last bit of “clinging-for-dear-life” peel ply was extracted (with much difficulty at times I might add!) I then used my ever trusty and ever awesome Perm-A-Grit tools to shape the foam edges of the 2 divots.

I should note that although the top was glassed with 2 plies, relatively there is so little mass in the U-shaped notched area that wraps around the fuel selector valve & bracket, that it was surprisingly “flimsy” for lack of a better word.  I decided to reinforce the center narrow area with a patch of BID on the bottom side, but alas I didn’t have any scrap pieces big enough . . . but then again, I did have one last piece of scrap CF hanging around.  I figured CF would provide even greater stiffness here so I threw it on there . . .  at the beginning of the 1-ply BID layup on the underside of the seat floor.  I know it may look a little unorthodox (read: nasty) but in my defense it’s the MGS epoxy’s fault, since if I had used EZ-Poxy you would have never known what it looked like!  hahaha!

Also, before I laid up the final large piece of BID on the underside seat floor, I also again laid up a scrap patch of approximately 2″ x 2″ BID over each divot & overlapping onto the foam to add reinforcement to these glass-to-glass only areas (5 plies of glass total when all is done).

It took a bit of time just to micro slurry the foam face, and then stuff thicker micro all along the mini trenches I had created along all 4 sides.  After the micro went on, to be honest, glassing up the large ply of BID was the EZ part.  However, getting the glass around the corners and sticking to the edges was a bit trickier, but in the end I got it all in place.

A number of hours later, after it all cured, I then razor trimmed the glass, sanded and cleaned up all the edges.

I have to say that I’m ecstatic with how the pilot seat floor plate layups came out!  I didn’t want bare foam on the edges that I would simply have to fill in with micro anyways, since if you’ve seen older plastic airplanes with bare foam edges on parts… well, they look really old, dry and unattractive (I guess that’s what folks say about us ‘ol dog pilots too, eh?!).

Anyway, here’s 3 pics showing the front, aft and side edges of the pilot seat floor plate:

I then of course mocked up the finished seat floor.  Ah, it fits great!

Here’s a closeup shot of the right underside divot where you can actually see the fuel pump frame jut-out (bottom pic) through the glass.  As you can tell, there’s plenty of clearance between the fuel pump frame and the seat floor plate.

Well, nothing left to do on this thing at this point other than try ‘er out!  So I set the seat floor in place, threw a towel and some padding on the pilot seat, grabbed my throttle handle quadrant and climbed in.

This first shot is exactly what I was aiming for!  The fuel selector valve is aft enough and high enough that I can actually easily see it and manipulate it during flight!  Hoo-ah!  Also, I should point out that my fuel selector valve bracket is only about 1/2″ max total farther aft than the stock plans fuel valve plate.  The difference: my valve is located at the very aft end of the plate, obviously about an inch higher, and not located center of mass on the valve plate as the plans valve is.

I then mocked up the throttle location to test it out.  I messed about with the throttle for a bit and determined that for me I had in fact picked the optimum location for this throttle quadrant setup.

Here’s a shot of the throttle handle/quadrant, fuel selector valve and control stick. Again, I’m extremely satisfied with the location, ergonomics and functionality of all these controls!

And here’s my parting shot of this post.  The throttle handle and quadrant in its planned left armrest location.

Again, this will be the last build post for the next couple weeks.  When I get back –renewed, refreshed and re-motivated– I will continue my quest to finish up the internal fuselage component configuration and install before starting on the nose & canopy!

 

 

Chapter 24 – Airplane baker man!

I started out today by pulling the peel ply and cleaning up the pilot thigh support ribs. I also cut out the glass from the mouse hole on the aft side of the right rib along with the overhanging glass from the layups.

I then trimmed the bottom of the right armrest to provide clearance and eliminate any rubbing on the fuel lines.

I also notched the bottom center of the left pilot armrest with a triangular opening to allow the armrest wall to fit over the pilot thigh support wedge duct when installed.  I also had to narrow the thickness of the wall on the outboard side of it that was adjacent to the air vent plenum duct in order for it to fit in its planned location.

I then got to work on shaping the pilot thigh support seat floor.  First, I copied the thigh support rib profile onto a template.  Then I used the template to mark up a scrap piece of OSB chipboard to cut out 4 thigh support rib jigs.

I then cut out the pilot seat thigh support floor piece from 3/8″ foam, and then clamped the 4 thigh support rib jigs to the bottom of the floor piece.

I then baked the jigged & clamped pilot seat thigh support floor piece in the oven for an hour at 280°.  In hindsight, it may have a been a bit too long to bake it, but in my defense there was no bake time listed in the plans!

I had to run out for a while after I turned the oven off and the floor piece started cooling down.

When I returned, I noted that there was a bit of waviness in the front & aft edges of the floor piece since the heating of the foam apparently produced some sagging in between the clamped rib jigs.  Moreover, these “scalloped” edges were significant enough that I thought about scrapping this floor piece and remaking another one.  But I don’t like wasting foam and to be honest, I kind of like the challenge of fixing a piece that’s less than perfect and make it work.

I pressed forward with the floor piece install and started working it until it proved to be unworkable, to see if it would . . . but it didn’t.

I wanted to lock in the CORRECT floor piece profile, so I decided to do a multi-part layup starting on the top of the floor piece surface (plans has you layup the bottom surface first). Since I needed to clamp both the front and aft edge to lock in the correct shape, I further decided to start with a large central ply of Kevlar –specifically to add puncture strength to a piece that gets stepped on every ingress & egress of the plane– and then add a strip of BID on both the front and aft edges after the center area floor piece profile was better locked into shape.  After these first pieces are laid up, I’ll of course lay up a ply of BID over the entire top surface of the floor piece.

As for the Kevlar layup, I started out by microing the surface of the floor piece top where the Kevlar ply will get laid up.

I then set the ply of Kevlar in place on the top of the pilot seat floor piece.

I then wet out the Kevlar.

And then peel plied the Kevlar layup.

Tomorrow I’ll continue to glass the pilot seat seat floor piece in my attempt to both get it installed, but also to straighten out some of the front and aft edge waviness that was introduced during my heating of the floor piece foam plate.  Still, I think it should be fine.

 

 

Chapter 24 – Thigh support ribs installed

Today was a very busy day, primarily in a non-build way.  Still, first thing this morning I got up and pulled the peel ply, knife trimmed, sanded and cleaned up the 1-ply BID layup on each side of the 2 pilot seat thigh support ribs that previously was bare foam.

I then made a shallow channel in the foam on the front edge of each rib. I quickly whipped up some micro paste and filled these shallow foam channels. I then covered the micro on the front edge of the ribs with a piece of peel ply, respectively.

I then left for a good 6 hours to help some friends with some heavy lifting at their community yard sale.

In the few-hour break between returning home from the yard sale and a planned outing for dinner and a movie with some friends, I quickly prepped, micro’d and then glassed the left side thigh support rib in place.  In a rare occurrence, since I was going to be late, I thought I’d get gritty and earthy and throw caution to the wind by NOT peel plying the left rib BID tapes.  (Note the Adel clamp mounted into the face of the pilot seat thigh support wedge duct)

A few hours later, I then prepped, micro’d in place and then glassed the right pilot thigh support rib.  Since I’ll eventual reinsert and glass the lower rib notch piece –and since time was not a factor– I decided to peel ply the right side rib install layup.

Here’s a wider view of the entire pilot seat thigh support rib affair.

Tomorrow will also be a bit lighter than usual on the build since I have to prep for going to Marco’s in order to help him as much as possible prep his plane for flying to RR.  I will say that my main goal for tomorrow is the thigh support cover plate that makes up a good portion of the bottom of the pilot’s seat.

 

 

Chapter 24 – Not much, thank you.

After doing some chores around the house, I had to run out rather unexpectedly mid-afternoon to help some friends that required some of my assistance.  I was out for about 6 hours and by the time I got home it was getting pretty late.

I wanted to get at least some glass “cookin’ in the oven” so I prepped & glassed the 2 pilot seat thigh support ribs on the one side of bare foam that each rib had.

Since I had cut out a small trough in the foam for the beginning of an elongated hole on the left rib, I had to decide whether to fill it back in or leave it.  I decided since I’ll be using wrenches during the installation and removal of the fuel selector valve to fuel pump main fuel feed line, I could use a bit of space between the rib and the line getting installed . . . so I left the trough.  I then angled the sides of the trough sloping inwards, and pressed on with glassing the ribs.

The glassing was uneventful with 1 ply of BID going onto the right rib, and 1 ply of BID on the left.  However, I did use an extra oval shaped ply of BID inside the trough and overlapping up over the edges.

Also, I didn’t micro the insert piece –that I cut out of the right rib– into the rib since I merely wanted to get a ply of glass laid up on it.  The hole that you see above the insert piece is where the right and left fuel sump tank feed lines travers the rib to connect to the fuel selector valve.  Once all is set and I’ve locked in the the fuel system configuration, I’ll micro the fuel lines into the rib and glass the insert piece back into place (unless I choose to glass it in from the get go).

I then peel plied the entire right rib glassed face and the edges on the left rib.  After assessing the layups the right rib looked fine, but the left rib glass was having a bit of an issue staying attached inside the trough.  I have to say, this is when I miss having my vacuum pump set up for vacuum bagging because this is a perfect scenario for using it. Especially since after messing around with it for a bit, I realized it wasn’t going to play nice.

So I pulled out the big gun.  I covered the trough half of the layup with Saran (plastic cellophane) wrap and gently wiggled a small 4-pound sandbag into the trough, which of course overlapped onto the majority of the trough side of the rib.  Sometimes taking this type of action is tricky since there may be an unknown issue that can’t be seen, but I figured keeping all the glass compacted and in place nicely with minimal delams or air bubbles would be worth the minor risk of something going awry.

Tomorrow will also be a light build day, but I do intend to at least get these ribs glassed into the fuselage.

 

Chapter 21/24 – 3rd times a charm!

Yes, 3 attempts it took bending aluminum tubes to make the fuel selector valve to fuel pump crossover line!!! . . . more on that below.

Today I started out doing some research on how to revive some old Chartpak dry transfer lettering sheet that I have.  Apparently, over long periods of time they lose their transfer ability and they simply don’t work. Well, I tried a few of the home brew remedies of the Web and was able to get the letters off at least, but I just wasn’t overly happy with them.

I wanted to use black characters on my red T-handle that I had designated as the Nose Hatch release handle, but it really didn’t look as good as I had envisioned.  So I punted and simply went with the fresh set of white dry transfer lettering that I have on hand.

As you can possibly imagine, it’s difficult enough to get these letters to line up on a flat smooth surface, and another thing entirely to do it on a curved contoured surface.  This is my excuse for the letter spacing not being perfect, but again –in my world– it’s darn close enough!

After getting the lettering transferred onto the red Nose Hatch handle, I took it down to the shop, taped it up and then shot it with about 6-7 coats total of matte clear.

In between the clear coats I started working on the fuel lines that connect to the Andair fuel selector valve.  Since I swapped out the valve fittings with the ones that I bought from Andair, which stick straight down vertically vs straight out horizontally, I hadn’t touched the fuel line connections since I was waiting until the fuel valve was mounted in it’s final position.

I was praying that I had enough length on each line to get to the fuel valve, since I had to lop off a decent amount of the curly-cue terminations of each fuel line in the craziness that I had undertaken to get them into the stock valve fittings while taking up as little space as possible.

In my new present tubing configuration I needed a decent amount of straight tubing just prior to the termination point to allow me to get the coupling sleeve on the line and still have room to flare it.  Yet just another reason I wanted to go with these new vertical fittings vs the curly-cue terminations… which made it really difficult to get a good flare with the coupling sleeve in place.

Well, apparently I had JUST enough tubing left to get to the new Andair fuel valve fittings. Still, it is all TIGHT and I will need to notch the lower right armrest a tad and contour the right underside edge of the thigh support top to allow for clearance with the right and left fuel feeds coming from the thigh support sump tanks to the Andair fuel selector valve.

I then cut and shaped the left thigh support rib to get it ready for glassing into place. Part of that prep involved pulling peel ply that I had applied when I laid up this piece back in mid-2012 … amazing!

Then, through the requisite trial and error fitting and sanding repeat cycle, I finalized the shape and got it into place.  My original location for this rib was very close to the stock location called for in the plans.

I then removed the fuel selector valve and its bracket to mount the fuel pump in place.  I then remounted the fuel selector valve and bracket.  I taped up the fuel selector valve because it’s a nice looking piece, and as I was mounting and removing it I noted that it was laying in a pile of tools, files, sanding blocks, etc. and for a minute thought that I had scratched it pretty good… I clearly needed to better protect the nice finish during the build process.

The fit of the left side of the fuel selector valve bracket and the inside of the left fuel pump frame is about as exact as could be.  Too close actually and I’ll need to trim the left side of the fuel valve bracket by at least 0.050″ to allow for clearance.  The clearance on both the instrument panel bulkhead attach bolts and the upper bracket attach screws is all good.

I then started the multi-hour process of shaping and terminating the 3/8″ aluminum tubing that makes up the fuel selector valve to fuel pump crossover line.  Amazing how many distinct requirements I had on such a short cross-connect tube.  First, I discovered I needed a distinct dogleg in the lower horizontal section of the tube to curve around the left tank feed line coming into the left side of the fuel valve.  Then there was the curve back, at about a 45° angle, to intersect the fuel pump fitting, which is a distinct angle change in comparison to the other side attached to the fuel selector valve.

Piece of cake, right?!  Yeah, after a couple of hours and definitely getting my tube cutting, bending and flaring practice in for the year!  Obviously I finally got it, and it’s the last bit of fuel line tubing bending I have to do on this plane! (I still have the brake cross-connect lines to do…)

Here are the previous 2 failed attempts  . . .

Another shot of the fuel selector valve to fuel pump crossover line, along with the other fuel valve connections.  Note the heater air SCAT tubing I set in place on the pilot thigh support wedge duct outlet.

I then spent a good hour getting the thigh support ribs configured and set in place.  As I stated previously, I had originally planned on having the left thigh support rib set in place at the plans location.  I even started notching the foam out to allow for the fuel pump’s left side fitting and the cross-connect fuel line to the fuel valve.  After pondering it for a bit I realized that it would just take too much work both in configuring, constructing and glassing the left rib simply to keep it in place at the plan’s location.  By kicking it outboard an inch to the left I eliminated all these issues & headaches…. so, that’s the spot!

On the right side there is simply no way that the rib can connect all the way from the aft side thigh support wedge duct to the bottom of the instrument panel bulkhead.  Not unless I never planned on removing the fuel pump.

Now, obviously hind sight is 20/20, but had I NOT used Clickbonds on the lower fuel pump mounting tabs and instead used embedded nutplates, I could have eliminated a LOT of my fuel pump mounting issues.  First, I could take the right side rib all the way to the bottom of the instrument panel bulkhead since I would have been able to slide the fuel pump in vs drop it in straight down. Even more helpful would be the fact that I wouldn’t have to remove the fuel valve bracket to get the fuel pump in or out…. the saving grace being that I don’t foresee having to be installing and/or removing the fuel pump a lot once the airplane is flying.

Here’s a wider angle shot showing all the fuel line runs in the pilot seat area, pretty much close to the original style as per plans, with some obvious distinct configuration tweaks I made on the fuel pump and fuel valve mounting locations.

I should note that the lonely Clickbond on the fuselage floor just aft of the fuel pump was originally for the 90 micron fuel filter supplied (and required) with the EFII fuel boost pump. I mounted this filter, and thus the Clickbond, prior to making my decision to go with the Holley Hydramat fuel pickups in the thigh support sump tanks.  Since the Hydramats filter to 15 microns, and I have one final 32 micron filter [as required by the Silver Hawk fuel injection system] at the firewall, there is simply no need for this 90 micron filter.  So…. out it went!

Between now and next week I do plan on continuing to knock out these build tasks, but admittedly it will start to slow the closer I get in heading down to Marco’s for our flying out to Rough River.  Hopefully I’ll see a bunch of you there!

 

 

Chapter 21/22 – Fuel Valve Installed

I started out today having a discussion with Mike from ElectroAir.  I had a few questions on the installation of the ElectroAir electronic ignition system, most being just crosschecks on what I was planning on doing and that I wasn’t going to screw anything up doing it!

There are a couple of connectors on their EIS (not GRT) Controller harness that I inquired about: the first connector –that I want gone– are on the wires running to the coils, and the second just a connector inexplicably (to me) placed on the controller’s ground wire.  The first will get replaced after I run the wires through the firewall to the coil, the latter connector will get removed altogether.  Both with the blessing of ElectroAir.

All this really relates to wire runs both in the hellhole and through the firewall.  That, in turn, relates to space required for wiring transiting holes through the firewall in the D-Deck / Turtle Deck / GIB headrest.

I then had a quick chat with B&C about the mounting requirements for the SD-8 Backup Alternator’s voltage regulator. The new electrical system requirement I picked up from them is that it’s highly recommended that I have a cooling fan for the SD-8 voltage regulator since apparently it runs a little on the warm side.

So, fan on the list to integrate into the GIB headrest.

I then integrated this new fan requirement into the electrical system, as well as moved the ElectroAir MAP sensor from the engine compartment into the Hell Hole, by reworking a number of my electrical diagrams.

Since I was on the computer upstairs updating my electrical diagrams, I took a good half hour to familiarize myself with Mike Beasley’s engine baffle templates.  I cut a few of the template pages into pieces so I could better get them organized, and after I had a decent understanding of what was going on I left them alone & headed down to the shop.

In the shop, I started off by determining the angle for the riser mount I’ll build to house the parking brake T-handle on the left side of the nose gear viewing window, and then a mirror one on the right for the nose hatch release T-handle.

After spending a good hour determining dimensions & drafting up some ideas on mounting these T-handles, I then got to work on cutting, forming, constructing, and mounting the top fuel selector valve bracket to the lower fuel valve bracket.

Although I plan on having some sort of support brace to assist in securing the fuel selector valve, I also had planned on the valve being mounted a little aft and a bit higher than the plans valve.  Thus, the mounting of my fuel valve would incorporate a significant stepped cantilever design for the upper valve bracket.

Allowing for this stepped cantilever design, I chose a 0.090″ thick piece of scrap 6061 for my stepped upper bracket. I don’t have a bending brake, so I resorted to clamps (one of which I broke!), 2x4s, and a couple of different hammers to bend this piece of metal to my will . . .  ha!  Moreover, (specifically for Marco) I started off by cutting the scrap 6061plate to its 3″ width using my Skil saw that was conveniently available.  For the curved aft end of the bracket I used my jig saw with a metal blade installed.

I then clamped & pounded, clamped & pounded <insert choice curse words here!>, replaced a broken clamp, and then clamped & pound some more.  I had my phone charging so I didn’t get any pics of this sequence, but suffice it to say it worked out well enough.  Again, it won’t win any beauty contests, but it’s strong as can be and it’s pretty darn straight to boot!

I then used my new Cleco clamp to help hold the bracket in place (in hindsight I won’t use a Cleco clamp on something with a nice finish –which ironically is why I chose this clamp– since it marred the finish. Since this plate will get covered or painted anyway, it’s a good lesson learned) and drilled pilot holes in the aft row of screw mounting holes, placing a Cleco in each hole as I drilled them.

Due to the width of the drill, I couldn’t drill the forward screw mounting holes without imparting an angle on each of the holes.

So I removed the Clecoed-together upper and lower bracket assembly and widened the screw mounting holes to 1/8″, with the subsequent Clecos getting mounted into each hole as it was drilled.

Due to my haste I also failed to get a shot of the 6 x K1000-8 nutplate assemblies that I drilled and riveted into place.  I had considered simply using 4 x #10 screws to secure the upper & lower plates together, but then after some thought I went with 6 smaller #8 screws.  Again, in hindsight I could have gone either way and now think the 6 screws may be a slight overkill, but it’s definitely secure!  Clearly, I needed 2 standard and 4 corner nutplates for this job.

Once the nutplates were installed, I then mounted the top fuel valve bracket to the lower. I’ll also state that the alignment deamons reared their ugly head here –despite my intense efforts otherwise– and somehow my bracket alignment got off kilter about 0.030-0.040″. To be certain, the left & right edges weren’t perfectly aligned when I started, but the front edge was.  So I ended up filing the front edge to make the edge straight and allow for it to fit flush against the lower instrument panel.

I then rounded up my installation instructions for the Andair fuel selector valve. Now, the Andair install directions would have you install the valve with the Left tank straight 90° left, the Right tank straight up, and the OFF position 90° to the right, like this: (L-9 O’clock, R-12 O’clock, OFF-3 O’clock). . . I changed that by rotating the valve a bit clockwise so the my Left & Right tank valve handle positions would be symmetrical, with my Left tank at the 10 O’clock position (45° left), my Right tank at the 2 O’clock position (45° right) in a  fashion, and my OFF at the 5 O’clock position (45° low right).

I then drilled the 1″ round center Andair fuel valve mounting hole, drilled the 3 each #10 screw mounting holes, and mounted the fuel selector valve.

I then removed the valve, countersunk the 6 x #8 bracket screws, and remounted the fuel valve bracket assembly onto the lower instrument panel bulkhead.

I then remounted the Andair fuel selector valve with its cover plate.

I then mounted the fuel valve handle.

And the parting shot of the evening: the fuel selector valve officially installed!

Tomorrow I’ll continue my pilot’s seat area build tasks.  To be clear, I can’t do the final install on the GIB area air & heat ducts until I figure out the cable runs and lengths to the 3 valves installed in the ducts.  To do this, I need to know the mounting configuration of the valve handles in the left pilot armrest.  Thus, in order to get the left armrest installed, I need to get the pilot seat thigh support ribs and cover in place.  So in an odd twist, the fuel valve I finished installing tonight has a direct bearing on me getting the GIB ducts installed!

 

 

Chapter 23 – Rabbit holes

Today I had a myriad of personal things to take care of early on.  When I got back to the build I really wanted to figure out some issues that I had run across when loading up the GIB headrest with components.

I had some questions for ElectroAir on their Electronic Ignition, and when I tried to call they were already closed.  When I checked out their site’s FAQ section, I noted their new requirement for mounting the MAP sensor: they now want it mounted on the cold side of the firewall, where before they stated to mount it on the hot side.  This new placement is in line with how GRT states their MAP sensor should be mounted, but throws a wrench in the works as far as how I have my MAP system configured…. so back to the drawing board.  Literally.

I didn’t want to just write a note and deal with this later, since the information I was collecting was all right in front of me.  I spent a few hours researching configuration options, figuring out fittings, and the physical install on each side of the firewall.  The end result was a couple of respective orders for very specific fittings (restrictor & barb), and an entirely new look of my MAP system by the time I was done.  In fact, below is a shot showing my MAP system about a year ago (top) and what it looks like now (bottom diagram).

In addition, although I don’t have a pic for this, I also spent a good hour updating my firewall components and pass-thru diagram, which has changed significantly from a year ago as well.

In prep for Rough River this year, I sent a note to Mike Beasley, Long-EZ builder extraordinaire, asking if he could bring his O-320 engine baffle templates he created a few years ago.  He had said I could get a copy, so I figured now was a good time.  Mike actually had soft copies of his templates, sent me those and I immediately went down to Staples and had them printed off.

Here’s a closer shot of Mike’s engine baffle templates.

While I was at it, I loaded up pg A14 of the plans on my thumb drive to have it printed as well.  I need to dial in and refine the shape of the rather rough-cut ribs that I have in my Strake Leading Edge kit from Feather Light.

I have to say all the copies came out about as perfect as could be from what I can tell (there are tick marks on pg. A14 and it did print out spot on).  With my manifold pressure system issues put to bed, I can now move on with the build and get back to my internal cockpit configuration tasks.

 

 

 

Chapter 22 – No turning back… now!

Haha!

I didn’t get ANY actual building done on the plane today!  Why?  Well today I got a nice delivery from the UPS bubbas . . . you gotta love people who bring you airplane parts!

Hmmm? . . . a big box from GRT Avionics.  This can’t be anything but good!

And what do we have here, 3 smaller boxes inside the big box.

Small box #1 revealed HXr EFIS accessories: GADAHRS, magnetometer, GPS antenna puck, OAT probe, and wiring harnesses.

I had already located my preprinted label stash and as each item came out of the box it got labeled with it’s 2-digit component ID.  I also wanted to check the fit of the GADAHRS on the top cross mounting shelf of the Triparagon: perfect fit!

The bigger of the 3 boxes was the GRT HXr EFIS itself. I bought the smallest HXr EFIS GRT sells –the 8.4″ model– since I wanted to conserve as much panel space as I could.  I figured it would fit well and still have exactly the same features as the large 10.4″ and 12.1″ models . . . actually more, since those models don’t have the optional touchscreen feature that I ordered on this unit!

You can see the top layer of the box contained more wiring harnesses, a thumb drive, and a display unit cross connect ethernet cable (that I won’t use since the Mini-X does not have an ethernet port… the displays will talk to each other via an RS232 serial pair).

And then I pulled out the centerpiece of my instrument panel: the GRT Avionics 8.4″ Touchscreen EFIS.  When I started this EFIS journey years ago, I’d never imagine that the unit I’d get was even more capable than what I was asking for.  I have to say that I’m extremely happy with the configuration, outlay and capability of my panel and avionics!

Here’s a shot showing the depth of the HXr EFIS.

And the back panel.

This shot gives you an idea of the actual size of the unit.  It’s not like I have gorilla paws, so this EFIS is a perfect size for a Long-EZ panel (in my opinion).

I’ll reflect back on how it is to plan something for literally years and then finally have it come to fruition.  This is my personal money shot right here.  Finally… my HXr PFD & the Mini-X MFD, together . . . where they belong!

I then opened up box #3, which contained all the wiring harnesses and engine sensors for the GRT EIS4000 Engine Information (management) System.  Since I needed a different MAP sensor that doesn’t come in any of the EIS4000 packages, I ended up getting the basic package and then just adding a couple higher quality sensors to the lineup.

And here’s the very capable EIS4000 control unit.  A lot of builders simply place this in their panel and call it a day, and it will work well that way.  But to spice things up a bit all you need is one little 22 AWG wire to port all that info via serial data into the HXr & Mini-X and you can see all the engine data in beautiful, colorful graphical representation.

I can’t even begin to relay how many phone calls that I fielded today.  So besides inventorying the new orders and crosschecking interfaces with components I already have on hand, I finished out the evening by “simply” figuring out the configuration of my GIB headrest (aka “component storage facility”) which will house the following (top down, CW):

  • Hobbs Meter
  • EIS4000 Control Unit
  • B&C SD-8 Backup Alternator Capacitor
  • B&C SD-8 Backup Alternator Voltage Regulator
  • B&C SD-8 Backup Alternator Self-Excitation Bridge Rectifier
  • Princeton fuel level control unit – Left Tank
  • ElectroAir EIS (Electronic Ignition System) Controller
  • Princeton fuel level control unit – Right Tank

(That’s all . . . at least for NOW!)

Oh, and let’s not forget the other item I also received in the mail today: my diminutive (cool in itself) MakerPlane AMX-2A Audio Mixer that allows me to take all my GNS480 system and NAV reporting messages, combine those with Trio AP audio reporting and CO sensor audio alarm, etc. and run it all seamlessly into my Dynon Intercom.  It has 10 channels so it can handle more than enough devices that I think I’ll ever throw at it.  And, as you can see, it’s literally the size of a 25-pin D-Sub connector backshell  [because it is one!].

Tomorrow I plan on getting back onto the build.  I’ll be honest though, as I start prepping for RR, and my 2 weeks of visiting friends in NC and VA, time will be in short supply.