Chapter 22 – Introducing PQD Bracket

First off, as you can see I’ve settled on the acronym PQD, Panel Quick Disconnect, to describe the connectors and bracket that I’ll be employing to make the task of removing the instrument panel infinitely EZier than without this configuration.  Although there will be some wires & components that will not be disconnected, either through their location just off the upper main Aluminum panel face, or because their wiring is not conducive to being split by a mid-point connector (eg Avidyne IFD COM plug P1002 & Dynon intercom wiring harness).

Speaking of the “upper main Aluminum panel face,” after some impromptu research I’ve decided that since I’m keeping a very large portion of the original panel in tact for strength behind the Aluminum panel face, that I’ll be using 0.063″ 2024T3 for the instrument panel. I was actually in the process of ordering that panel from ACS, when I double checked my spreadsheet and lo & behold, I had a spare 2′ x 2′ panel on hand from years ago.  Woo-hoo!

Ok, back to the PQD.  I had originally ordered a 1/8″ thick 2-1/2″ x 2-1/2″ angled piece of 2024 from McMaster-Carr quite a while ago thinking that I would hang a bunch of stuff off these cross shelf overhangs in the same fashion that I’m doing now with the clearly much smaller sized 1″ x 1″ angled aluminum overhangs.  This angled aluminum extrusion was just too big & heavy to use in any reasonable quantity, plus as my Triparagon design matured I just didn’t have a need for it.  So into the massive spare pile of aluminum it went.

Then when I was finally hit between the eyes seeing Paul Dye’s panel on the VAF forum as I was trolling for pitot-static info, I finalized my decision to make my panel fully & EZily removable. So I had to get serious on both the quantity & type of connectors to use and where they would reside.  I had had a nascent thought all along of a drop down bracket on the aft right corner of the Triparagon cross shelf IF I did the fully removable panel mod.  Well again, it was time to get really serious so out came the big gun: the 1/8″ thick 2-1/2″ x 2-1/2″ angled 2024.  If you remember I posted a few days ago, over the Thanksgiving holiday, a mockup of my connectors on the end of this massive 2′ long piece of aluminum. With my electrical connections confirmed, and with the only mod to the actual connectors being that I swapped out the 19-pin AMP CPC connector for a higher capacity 24-pin connector (same diameter), I was ready to install the J3, J4 & P6 connectors into the PQD bracket, and of course make the PQD bracket itself.

I started by marking the connector outlines on the angled extrusion.

Designing Panel Quick Disconnect (PQD) connector bracket

I then used a hole saw to drill the 1-1/2″ diameter hole for the P6 AMP CPC connector.

Making PQD connector bracket

Of course I had to check the fit…. looking good so far!

Testing P6 connector fit in PQD bracket

Then came the odd shaped 37-pin & 15-pin D-Sub connectors.  I figured this would be a total hand-jam custom build process (“custom” means it works fine, but it ain’t always pretty!).  I drilled some small starter holes, focusing especially on the corners.

Drilling out D-Sub slots in PQD bracket

I then expanded out the center area holes with a large diameter drill bit, which is the same diameter as the width of the D-Sub connectors.

Drilling out D-Sub slots in PQD bracket

I then employed my jig saw –and a few expletives!– to finalize the cutouts for the D-Sub connectors.  Here’s a shot of the initial rough connector cutouts in the beginnings of the PQD bracket.

Connector holes made in PQD bracket

And another shot after I cut the bracket out of the angled 2024 extrusion (it was raining so I plunged forward using my Skil saw to cut the bracket out!).

PQD Bracket

I then test fitted the connectors in the PQD bracket.

Connector test fit in PQD bracket

Here’s a shot of the backside of the connectors test mounted into the PQD bracket.

Connector test fit in PQD bracket

I then took the PQD bracket upstairs and mocked it up on my Triparagon cross shelf. After finalizing the mounting location for the PQD bracket on the cross shelf, I then digressed a bit from the PQD bracket and figured out where my first round of lightening holes would go on the cross shelf.

Marking Triparagon cross shelf lightening holes

I took the cross shelf and the PQD bracket down to the shop and proceeded to drill the mounting holes for the bracket into the bracket tab and the cross shelf.  I then added 3 K1000-8 nutplates to the PQD bracket mounting tab.  As you can see, I also drilled 4 lightening holes in to bracket’s mounting tab.

PQD bracket nutplate mounts

Here’s a view of the top of the PQD bracket mounting tab, with the flush rivets of the 3 K1000-3 nutplates visible.

Mounting edge of PQD bracket

I then diverged from working on the PQD bracket for a bit and drilled out the first round of a bunch of lightening holes into the Triparagon cross shelf.  After finishing round one of lightening holes, I then went back to work on the PQD bracket and drilled countersinks for each of the 3 -8 screws into the top of the Triparagon cross shelf (shown 2 pics below).  I then mounted the PQD bracket to the cross shelf.

PQD bracket mounted to cross shelf

I then test fit the cross shelf back onto the vertical Triparagon plate.  Note the 3 countersunk -8 screws securing the PQD bracket into place.  (Note: while I was drilling the PQD bracket mounting holes through the mounting bracket into the cross shelf, the bracket misaligned slightly.  Nothing earth shattering, but definitely a slightly-sloppy mounting AND a loss of cool points!)

Cross shelf test fit with PQD bracket

After I finished with the PQD bracket mounting on the Triparagon cross shelf, I headed out the door to an auto racing shop just across the river in Maryland that sells some high end stuff.  I knew that they sold the same quick disconnect fittings that I’m using for my pitot-static system, so I wanted to take a quick break from the build and take a gander.  Well, it had been raining all day, but there seemed to be a lull.  So I grabbed the keys to the shed, pulled out my table saw and trimmed down the 1″ x 1″ angled 2024 aluminum extrusions that will serve as my Triparagon cross shelf mounting tab overhangs.

I trimmed these angled extrusions down on the sides that will mount to the front underside edge of the Triparagon cross shelf.  I took 0.4″ off, with the obvious resulting width of the top horizontal extrusion arm being 0.6″.  This took all of 10 minutes, and it actually started sprinkling again as I was putting the saw back away in the shed.  With my overhang extrusions cut, I was then off to the racing shop in Maryland.

As a reminder, besides simple weight savings, I wanted to trim down the left side angled extrusion, specifically, to allow me to mount the M760REM COM2 radio about 0.4″ forward on the left underside of the Triparagon cross shelf.  This served to better deconflict the mounting screw placements between the COM2 radio and the GRT GADAHRS that’s mounted on the top side of the cross shelf.  The right extrusion was merely along for the ride since I might as well make them symmetrical, right?!

1" x 1" Triparagon cross shelf overhangs trimmed

Back from the racing shop, and my quest to replace the #40 drill bit that I broke (to no avail), I got back to work. After I collected up the right sized bits for drilling the connector mounting holes into the PQD bracket, I decided to take yet another slight detour to finalize a task that needed finishing: the right-side avionics wall bracket for the P3 & P5 connectors.  I drilled out the 8 total connector mounting screw holes and then did a final cleanup on the bracket by sanding down the edges and ridding it of excess glass fibers around all the holes.  I then test mounted both the P3 & P5 connectors.  I brought down the Trio A/P wiring harness from upstairs to test fit the other side of the P3 connector [confession time: I spent a good 10 minutes looking for that darn P3 connector just to finally realize that I had mounted it to the end of the Trio wiring harness pitch servo cable!].  You can see that I also set the 2 white auto trim wired into the back of the P3 connector as well.

P3 & P5 connector bracket completed

Here’s a longer shot of the P3-A/P Pitch Servo and P5-Infinity Stick Grip connectors test fitted and mocked up in place.

P3 & P5 connector bracket completed

Moving on with more connectors, I then mocked up the PQD connectors P6, J3, and J4.

PQD bracket mounted - view from below

Since I was holding the camera down low taking low-to-high angle shots of the PQD bracket through the right leg hole, I took a few rounds to ensure that I got a good pic.  I had to leave this one in the mix since it looks like something out of Star Wars with a pure beam of energy coming out of the back of the P6 connector.  That’s right folks… no wires for me! Just pure energy transfer in my ship!  HA!

PQD turned on...pure energy!! ha! ;)

Here’s another shot of the PQD bracket and its connectors.  Note that although I originally wanted to mount the D-Sub connectors on the aft side of the PQD bracket (which would be the forward side of the plane), it initially appears that the connection hardware with the mating side D-Sub connectors will be tough to do if I left them aft-bracket-side mounted. I’ll play around with the hardware a bit, but I think that this will most likely be the mounting configuration for these connectors.

PQD bracket - top view

An issue that I noted was after I test fitted the aft side P6 connector’s cable clamp: Hmm, don’t think it’s going to fit since the gap spacing between the cable clamp and the panel is only about 2-5/8″.  It would most likely actually fit, but then of course all the wires would exit and then immediately have to take a hard 90° turn to get to their final destination.  Not good.  So . . .

Uh-oh... Eh, a bit of a space problem!

Be gone vile & wicked cable clamp! (said in thick British villain voice… sorry, my Brit Canardian Peeps.  ha!)

Ok, much better!  As you can see with the P6 connector cable clamp removed I get about another 1.5″ clearance and 4″ spacing overall.  Still slightly tight, but since the GRT HXr EFIS is low profile on the backside this is EZily workable.

Ah, that's better... Bye-bye cable clamp!

And yet another shot showing all my current Avionics Bay connectors.

Connectors, connectors!

I reordered my blog post pics just a bit to make the topic flow a bit EZier to follow.  If you looked closely in my Avionics Bay pic above, you may have noted that I drilled a hole into the triangular panel support and added another RivNut for the second & final Adel clamp that will also be used for the Infinity Stick Grip cable routing from the stick to the P5 connector.  I also added a couple of layers of BID on the bottom side of the support triangle to beef up the RivNut mounting.

RivNut in for stick cable 2nd Adel clamp

Back on the Triparagon cross shelf, with the PQD bracket configured & installed, I then started in on some of the final pieces parts (aka “CrackerJack Bits”) that I need to mount to round out the final electrical system components install on the Triparagon.   I found a good spot for the Piezo Warning Horn on the right underside of the cross shelf. I mocked it up, ensuring it had good clearance with the vertical Triparagon components (it’s close to, but not touching, one of the mounting screws to the right side AG6 warning annunciator). I drilled the holes for #6 mounting screws and then countersunk the 2 screws on the top side of the cross shelf.

Piezo warning horn mounted on right side

Here’s a closer shot of the mounted Piezo Warning Horn with the #6 mounting screws installed.  I used standard nuts on the screws to mock up the warning horn & make it EZily removable.

close up of warning horn mount

I then test fitted the Triparagon cross shelf onto the vertical plate to double check the clearance between the warning horn and other Triparagon components.  In the pic below you can see the 2 countersunk #6 screws, and the warning horn itself through the lightening hole.

Piezo Warning Horn #6 CS screwsHere’s a final shot of the mounted Piezo Warning Horn on the right underside of the Triparagon cross shelf (pic taken from the front of plane).  You can see that it’s close in line to the wiring bundles that will spew forth from the PQD bracket, but also clearly not in the way either.

Piezo warning horn mounted

I then brought my cardboard component mockups that I made a year or so back to check out their general fit on the Triparagon cross shelf.  Below you can see the GRT GADAHRS (their new term for their new AHRS) and the Trig TT22 Transponder behind the GADAHRS.

GADAHRS & XPDR mocked upAnother shot of the cardboard GADAHRS & XPDR mockups.

GADAHRS & XPDR mockups

Just an idea of the fit of the Trig TT22 Transponder on the Triparagon cross shelf.

Trig XPDR mock up box

And the cardboard GADAHRS and XPDR on the Triparagon cross shelf with the rest of the left side Triparagon in view.

The whole shebang

Since there’s forecasted high winds tomorrow, and thus no flying, I’ll continue my quest to finalize the Triparagon cross shelf and resident components install.  I will be doing some more sideline wiring on my components since currently they’re EZ low hanging fruit, and don’t conflict with other parts of the build (like so many other build actions do at this point!).  It doesn’t look like to much longer before I’ll be back on the . . .  Yes, WHEEL PANTS!

 

Chapter 22 – 3 Cheers for Karnaugh!

Yep, today I employed a rudimentary list-form version of the Karnaugh map, or k-map to figure out the circuits going to/from the respective A & B sides of the 3 connectors that I’m using to enable a fairly quick-disconnect of my instrument panel.  If you’re wondering what a k-map is, it’s used in Boolean Algebra and reduction to reduce a multitude of circuits down into the least number of circuits possible and still get all the correct functions out of an integrated circuit chip.  Or, as that Internet thing puts it, “Karnaugh mapping is a graphic technique for reducing a Sum-of-Products (SOP) expression to its minimum form.

Although not overly difficult, it was of course time consuming to go through literally every wire & component to ascertain its relationship to the panel.  Moreover, since I had finalized all the I/O requirements (yes, this is still an airplane building blog, NOT a computer forum… ha!) for my throttle handle switches, I realized as I was building the new connector diagrams that with a little internal (to the throttle handle) consolidation of 3 ground wires, that I only needed exactly 19-pins for the throttle handle connector.  Thus, I could then swap out the 24-pin connector that I had planned on using for the throttle with the now “old” 19-pin connector that I had on hand for the recently put-out-to-pasture GIB Infinity control stick (AKA “the really expensive spare control stick”).  The new configuration for my 3 connectors (I’m going to have to come up with a reference name to identify these things! . . . I’m leaning toward the “PQD (Panel Quick Disconnect”) is as follows:

  • P6: 24-pin AMP CPC – Thick wires/high power & ground connections
  • J3: 15-pin D-Sub – Thin wires/low power & ground connections
  • J4: 37-pin D-Sub – RS232 data & low power transfer connections

With the PQD connectors (trying it out . . . ) squared away I then decided that before I put away the Trio Pro Pilot autopilot wiring harness I would cut & terminate the shielded 4-wire cable for the pitch servo.  I took it down to the shop and determined the required length.  I then cut it WAY shorter than how it comes from Trio.  The excess cable that I cut off is visible above the harness in the pic below (post terminated connectors).

Trio autopilot wiring harness

As with shielded cables, I carefully stripped the outer cable jacket and consolidated the shielding wire to one side.  After twisting it and cutting it down to about a 0.3″ pigtail, I then soldered a piece of black 22 AWG wire to the pigtail.  I then terminated the black pigtail wire in tandem in an AMP CPC socket with the identified ground wire of the 4 wires. I then terminated the other 3 wires with sockets as well.  Also, I added a piece of black heat shrink over the soldered joint to protect the joint and add a bit of strength to the cable for when I eventually set the connector cable clamp in place.  Finally, as I did with the roll servo cable, I performed an electrical continuity check on each wire to ensure my connector terminations were good.

Cut and terminated pitch servo wires

This concludes the connector upgrades for the autopilot’s pitch & roll servos, and the wiring harness pitch & roll servo cable feeds.  The roll servo connector (below right) is pretty much complete, but I haven’t finalized it 100% since I will have to remove the connector to route the cable down the fuselage side & through the firewall.  As for the pitch servo cable (below left), I still need to terminate the 2 autotrim wires and install those into the connector when it gets installed “for good” in the plane.

AP pitch servo and roll servo connectors

The last task of the evening was to review the mounting spacing of the Trig TT22 Transponder on the topside of the Triparagon cross shelf since it could potentially affect the mounting of both the front 1″ overhang on right-side cross shelf, as well as the PQD junction mount on the aft right side of the cross shelf (both on the underside of the cross shelf).

It’s dark & cold out right now so I’ll wait until tomorrow to cut the PQD Aluminum angle mounting bracket, as well as narrow down each of the forward 1″ x 1″ angled Aluminum cross shelf overhang tabs (for the CrackerJack parts) by about 0.4″, resulting in 0.6″ wide top arms.  I’ll also assess all the wiring going through the PQD connectors to ensure the wires are physically inserted in a logical manner to keep the wire bundles as free-flowing and stress free as possible.

 

 

Chapter 22 – Sloggin’ it out!

Today I started out by finalizing my pitot-static system plan.  I still need to make some phone calls tomorrow to some of system vendors to ensure I’ve got the most optimized configuration for hooking up the pitot-static lines on their respective systems, but beyond that I’m pretty much done.  I’ll be dropping an order to Stein here soon and it will include the remainder of the parts I need to complete my pitot-static system install.

Pitot-Static System

In addition the pitot-static system, I also reviewed & assessed my recently added Triparagon connectors that should allow me to remove the instrument panel fairly easily.  I found a few more issues that made me add the Trio autopilot’s wiring harness to the list of components that require me to simply remove the connector.  The main issue with this harness is that there are shielded wires that run all the way back to the roll servo.  Clearly these are not easily removed, and I’m sticking to Stein’s advice (because I agree!) to NOT add connectors in the middle of shielded wire runs.  Thus, this requires me to remove the Trio autopilot’s connector and leave it in the plane when I remove the instrument panel. In short, I made a lot more progress on the concept of running all the instrument panel components’ wires through connectors to allow EZ removal of the panel.

Later on, I figured I would get some wiring done while I was watched football.  Since I had just had the Trio autopilot wiring harness out, I decided to re-terminate the roll servo pins with AMP CPC pins vs Molex, and add the AMP CPC connector housing.  I’m not messing with the pitch servo since it needs to be cut significantly shorter and I need to get a good measurement for that.

Trio autopilot wiring harness

The pic below shows how the connector pins looked before I started.  Again, I cut the Molex pins off and reterminated the wires with AMP CPC pins and then mounted the connector housing for the roll servo cable.

New A/P roll servo AMP CPC connector

Continuing on, perhaps a little ironically I removed the 9-pin D-Sub connector from the roll TRIM servo and swapped it out with a 4-pin Molex connector I got from Stein.  As you probably know, I’m not a huge fan of Molex connectors, but I figure any roll trim servo failure is fairly benign in the operational realm of flying a Long-EZ.

"Old" Roll TRIM Servo connector

I started by cutting off the D-Sub connector as close to the connector housing as possible.  In both pics above and below you can see the 4-pin Molex connector housing.

Swapping Roll TRIM servo connector

I then reterminated the wires with mini-Molex pins.

New Roll TRIM servo Molex connector pins

And then snapped the pins in place into the Molex connector housing.  BTW, this connector is J6.  I’ll of course wait to terminate & add wires to the other half of the connector when I actually install the roll trim servo.

New Roll TRIM servo Molex connector

My last action of the evening was to rewire the wiring harness for the TruTrak ADI.  As I was taking inventory of all the wires, which included digging into the manuals, I noted that the wires on the TT ADI’s wiring harness connector were simply HUGE!  Although the installation manual calls out for 22 AWG wiring, these wires range from 14 to 18 gage… way too big!  Since the wires were soldered into the 9-pin D-Sub connector, I simply created an entire new TT ADI wiring harness D-Sub connector with crimped pins.  I of course used 22 AWG wires for the new harness.

Rewiring TruTrak ADI wiring harness

Here’s a closer shot of the new TT ADI wiring harness (red, black & yellow) that will replace the old one (white wires).

Rewiring TruTrak ADI wiring harness

Tomorrow I’ll finish the plan for the wiring, finalize the positions of the airspeed switches and other Triparagon cross shelf mounted components (“CrackerJack parts!”) and attempt to get the Triparagon cross shelf mounted.  I’ll most likely order the pitot-static parts as well after talking to a few equipment vendors.

 

 

Chapter 22 – Unraveling the mystery

Over the past few days during the Thanksgiving holiday I’ve actually been getting a fair amount of electrical system documentation, planning & system design work done.  Some things I’ve done, like taking the time out to figure out the wiring & pinouts for the Infinity pilot control stick buttons, switches & wires, is pretty much a known quantity and simply needed to be completed & checked off the to-do list.

Determining P5 connector pinouts

But the pitot-static was a different animal entirely. I had some pieces parts on hand, but I really needed to get educated on pitot-static systems before starting out.  During my research I ran across a very nicely detailed post on the VAF forum from Paul Dye (editor of KitPlanes mag) concerning his pitot-static system.  In the post he not only described his pitot-static system, and the advice that Stein (from SteinAir) –who we know is a genius on all things panel related– gave him, but how he also devised his pitot-static system, and in turn his electrical system, to allow for the panel to be removed EZily.  Hmmm?!

I played around with designing my pitot-static system with the intent to get it documented in PowerPoint and on paper, but have not gotten around to either yet.  Although I pretty much have the pitot-static system designed in chicken-scratch form & in my head, as you can see below (the diagram below was summarily stolen from a guy asking questions on his p-s system that posted it to VAF…I’m merely modifying it to suit my needs!).  But the panel removal idea –one that Marco and I have discussed non-specifically many times– began to gnaw at me more & more each passing day over these past few days.  It was definitely germinating in my brain.  One overriding reason is that if I could pull it off, it could literally change the structure & process of how I build the nose of my plane.

Planning/Configuring pitot-static system

So today I spent the entire day taking inventory and listing out every single wire that comes off the panel mounted avionics, instruments, warning lights, buttons, switches, etc. I determined what connectors would need to stay connected, and which ones must be disconnected for the panel to be removed.  I created a whole new series of connector designators for the D-Sub and Molex series connectors: J1 – Jn, as compared to the current series of the AMP CPC connector series: P1 – Pn.  

After hours of collecting this data, and determining that it could be done, then I got to the business of updating the majority of my electrical diagrams to reflect these new intermediate connectors.  I determined a couple of things, at least initially:

  1. The majority of switches will be on separate sub panels that will be removed from the panel before it is removed.
  2. The Avidyne P1002 communications connector and the Dynon intercom connectors will have to be removed and stay on the plane side due to the multiple cross/inter- connects to components and the shielded wiring.
  3. Given the factors above, I determined the number of pins required could be provided with 37-pin (J4) and 15-pin (J3) D-sub connectors, and utilizing the 19-pin AMP CPC connector (P6) that I had previously planned on using for the GIB stick grip.  These should give me enough pins for the panel wiring, with some extra slots.  The AMP CPC (P6) and 15-pin D-Sub (J3) will handle primarily power & ground wires, while the 37-pin D-Sub (J4) will handle primarily signal (a ton of RS232) wires.

Panel removal electrical connectors

Of course I need to confirm and refine my plan, but with this in hand and the finalizing of the pitot-static routing plan, I’ll be able to finalize the component placement on the Triparagon, get the top cross shelf and side mounting tabs cut and lightening holes drilled. I’ll also be able to roll these new factors into the design of the top nose structure and see how it effects the forward canopy skirt.  Tomorrow will be a light build day, but I do plan on getting a few hours more done on this stuff.

 

Chapter 22 – Back on the shelf…

I had an Instrument flying lesson this afternoon, so I knocked out a couple of things before the lesson and then a bit afterwards.

I started off by cleaning up something I forgot to mention yesterday: the Rivnut that I installed with flox into the lower frame of the instrument panel to mount an Adel clamp for the blue multi-wired Infinity stick control cable.  I drilled the hole using my flexible drill bit adapter and a 1/4″ drill bit.  Then when I laid up the 2 plies of BID on the top of the AMP CPC connector bracket, I floxed the Rivnut into place.  As per usual, I used a small piece of duct tape on each end to keep the flox from gumming up the threads.

This morning I removed the outer piece of duct tape.

Floxed Rivnut for control stick Adel clamp

And then test fitted the Adel clamp.  I’ll be installing one more of these Adel clamps for the control stick cable on the outboard/front edge of the instrument panel corner reinforcement wedge I installed a while back.

Floxed Rivnut for control stick Adel clamp

I then spent a good half hour redrilling the holes and cleaning up the 2-ply BID layup on the topside of the AMP CPC connector bracket.  In the left pic below, besides the cleaned up connector bracket you can see the freshly mounted lower control stick cable Adel clamp, and the instrument panel corner reinforcement wedge where I’ll install the second control stick cable Adel clamp.

I then quickly test fitted the control stick cable AMP CPC connector (P5) after sanding the underside of the bracket in prep for glassing.  You can also see I bagged up & taped the AP pitch servo to keep it epoxy free.

AMP CPC bracket top 2-ply BID cured

AMP CPC bracket connector test fit

After adding a flox fillet at the corner of the bracket & the fuselage sidewall, I then laid up 2 plies of BID on the underside of the AMP CPC connector bracket.

AMP CPC bracket underside 2-ply BID layup

I finished off the layup with a strip of peel ply, primarily focusing on having a good glass transition on the sidewall glass (read: no fiberglass barbs playing “gotcha” while working in the avionics bay!)

AMP CPC bracket underside 2-ply BID layup

I then left for my flight lesson… [flew 3 instrument approaches under the hood… beautiful day for flying and the 30 seconds I saw here & there out from under the hood were an awesome sight! haha!]

Upon returning from flying, I spent another good half hour razor trimming the 2-ply BID layup on the underside of the AMP CPC connector (seen in last pic this post).

I then clamped the right side angled aluminum Triparagon shelf mounting bracket in place, with a scrap piece of 0.090″ aluminum as a spacer, to the screwed-in-place left side bracket.  I used my drill press to drill the 3 screw holes through both the angled aluminum bracket and the Triparagon cross shelf.

Drilling Right side Triparagon shelf screw holes

I then riveted 3 each K1000-3 nutplates to the right side angled aluminum mounting bracket, and countersunk the 3 screw holes on the top side of the Triparagon cross shelf. As shown in the pic below the cross shelf weighs in at 0.6 lbs, so current total weight of the Triparagon structure is at 1.3 lbs gross.  I’m certain I can knock half of the shelf weight off with lightening holes, so I expect the total weight for the installed Triparagon structure to be around a pound.

Triparagon shelf screw holes - nutplates installed

I then test mounted the Triparagon cross shelf to the installed Triparagon vertical plate. So far so good.

Triparagon cross shelf test fit

I then took the cross shelf upstairs & diagrammed out the installation location for the M760REM COM2 radio.  To set up the following discussion below, I’ll point out that I plan on having a 1″ x 1″ piece of angled aluminum mounted to the bottom front edge of the Triparagon cross shelf, one on each side of the vertical plate, for mounting what I now call the “CrackerJack Parts” (small airspeed switch size components).  To be clear, these angled aluminum pieces are NOT shown in the diagram below.

Triparagon Top Component Shelf

Now, to optimize the installation of the radio in relation to the GRT GADAHRS (see above), I decided that I need to trim the cross shelf’s front side angle brackets horizontal sides down by 0.4″. In other words, the vertical arm of each front angle bracket will be 1″ with the new trimmed horizontal arm (that mount to the the underside of the cross shelf) being 0.6″ wide. This will allow me to move the radio forward on the left underside of the Triparagon cross shelf, and provide better clearance between the mounting screws of the radio & GADAHRS.  It will also allow for the aft edge of the Triparagon cross shelf to provide more of a protective overhang for the radio’s antenna & DB15 connectors.

I’ll work a bit on the cross shelf tomorrow, but for the most part I’ll be heading into Thanksgiving holiday mode over the next few days.  It is simply imperative that I tend to my duties as the gregarious socialite!  hahaha!

 

Chapter 22 – Triparagon Shelf

I didn’t go flying today due to high winds, so I started off with a little cleanup action on the nose gear wiring harness.  I’ve had a bundle of excess wires sitting on top of the NG30 cover for eons now and decided it was time to clear them off.  Also, instead of using butt connectors I opted for a more “elegant” solution and spliced the wires using a pigtail to secure the stripped ends of the individual wires together before soldering them.

Here is the first set of 3 that I did this morning.  You can see the long 3-4 wire pigtail that I teased out of the stripped red wire on the left before cutting the rest of the stripped wires short in length to match the white wire on the right.

Splicing nose gear power wires

I then used the pigtail to secure the 2 wires together.  I could have used a wire or two less on the pigtail and also cut it a bit shorter, which added to the slight excess in the wrap. No worries though, it still worked great.

Splicing nose gear power wires

I then soldered the wires together.  I actually added just a tad bit more solder after I took the pic below.

Splicing nose gear power wires

Here’s wire set #2 getting spliced . . .

Splicing nose gear power wires

. . .  then soldered.

Splicing nose gear power wires

And wire set #3 completed in the same fashion.

Splicing nose gear power wires

Here you can see all 3 wire sets spliced & soldered together.  I used shrink tubing over the joint for added joint strength, then simply used the label as a second layer over the shrink tubing for even more added strength.  After I finished with the shrink tubing & labels, I then hooked up up the battery leads and ran the nose gear up & down a bit to ensure the splices were carrying current, which they did.

Heat shrink labeled spliced nose gear power wires

This morning at breakfast I drew up a plan for a bracket that would hold the AMP CPC connectors P3 (A/P pitch trim servo) and P5 (pilot stick grip) in place on the avionics bay sidewall.

I decided to go ahead and knock this out so that the glass would be laid up and curing overnight.  For the bracket material I figured I would use some leftover 1/16″ thick G10 that I had on hand.  I was going to use some of my 1/16″ brown phenolic at first, but it cuts a little easier than the G10 so I’m saving it to continue using for my nutplate backers.

G10 plate for AMP CPC connectors

So I cut off a 3.5″ long piece off the 2.2″ wide strip of G10.  I then rounded the front corners.

G10 plate for AMP CPC connectors

And drilled 2 pilot holes to mark the center of the larger holes.

G10 plate for AMP CPC connectors

Which I then drilled next… along with the small #40 & #6 size screw holes, respectively of course!

G10 plate drilled for AMP CPC connectors

After finalizing my mounting location, I then 5-min glued the bracket into place on the sidewall.  I screwed the aft corner of the bracket to a clamped 2×4 piece to keep the bracket aligned while the 5-min glue cured.

G10 plate 5-min glued for AMP CPC connectors

While the AMP CPC connector bracket 5-min glue cured, I got to work on the Triparagon cross shelf.  I marked out where the GRT GADAHRS will get mounted along with the centerline, then configured the angled mounting bracket locations.  I marked the mounting screw locations on the angled mounting brackets, then took the angled brackets and the cross shelf down to the shop to drill the holes.

Drilling Triparagon top shelf angle bracket

After I got the 3 mounting screw holes aligned & drilled, I then riveted nutplates to the left angle bracket.

Triparagon top shelf angle bracket nutplates installed

I then countersunk the 3 left side screw holes on the top of the Triparagon cross shelf and then screwed the shelf to the left side angle bracket.

Left side Triparagon top shelf angle bracket

Here’s a top view of the 3 left side countersunk screws.

Left side Triparagon top shelf angle bracket

I then quickly mocked up the Triparagon cross shelf.  Again, I really am liking how the Triparagon is coming along.

Triparagon cross shelf

My last official act of the evening was to stop making noise and start making some fumes… epoxy fumes that is.  I whipped up some epoxy and laid up 2 plies of BID on the top side of the AMP CPC connector bracket.  I did use a flox fillet so the glass would transition well between the wall and the bracket. And of course I finished off the layup with some peel ply.

P3 and P4 AMP CPC connector bracket

If the winds stop acting up I’ll be flying tomorrow afternoon.  Still, tomorrow I will try to get the Triparagon cross shelf mounted, as well as the bottom/final glass laid up on the connector bracket.

 

 

Chapter 22 – Wires, wires, wires!

I started out today by trimming the reglassed aft lower Triparagon nutplate mounting tab with the Fein saw.  I then cleaned it up by sanding down the edges and then redrilled the hole to allow me to thread in the mounting bolt, which as you can see I’ve done below.

Lower aft Triparagon mounting tab

I then labeled the power wires coming off my Atkinson pitch trim servo motor with heat shrink labels on both ends of the wire.  As you can see I had to unravel the twisted wire then retwist them back together after the labels were on.  However, since the servo motor came from the supplier with these wires, I wanted to test them to see how they held up under heat & fire.  I snipped a test piece off and tried to burn it with a lighter for a good couple of minutes to no avail.  With my impromptu wire fire rating test complete, I then went ahead and affixed the labels and retwisted the wires.

Atkinson pitch trim servo power wires

With all my mounting tabs good at this point, I then brought the Triparagon down to the shop and officially mounted it!  Here’s a shot of the right side Triparagon.  Note the 2 white wires circling around to the right side of the pic and laying atop the Trio A/P pitch trim servo are the 2 Autotrim wires that interface with the servo.

Mounted Triparagon & Volt Reg - Right side

A shot of the right side Triparagon.  Again, after all the wires are in place I’ll do some major cable management on this rats nest before it flies.

Mounted Triparagon & Volt Reg - Right side

Here’s the left side Triparagon.  As I mentioned before, I’m extremely pleased with how this turned out.  My next task will be to configure & mount the top cross shelf that will primarily hold the GRT GADAHRS, Trig TT22 Transponder and M760REM COM2 Radio. Also attached to the upper level will be 3 airspeed switches, the Gear & Canopy Warning module, the piezo warning buzzer, and possibly some pitot/static manifold blocks.  All these components I just mentioned above make up virtually the entire electrical system other than those components that will be mounted on the Instrument panel.

Mounted Triparagon & Volt Reg - Left side

In the pic below of the left side Triparagon, you can see the Voltage Regulator in the upper left of the pic (again, mounted to F22, not Triparagon), the Endurance Buss (E-Bus/EB), TCW Smart Start module (SM), and the Autotrim components on the forward edge.  Note in the middle of the pic you can see the twisted red & black wires coming from the Atkinson pitch trim servo motor, terminated with small FastOn connectors to mount on the Autotrim relay (RP) tabs.

Mounted Triparagon & Volt Reg - Left side

Here is a close up view of the Trio A/P Autotrim components: a bridge rectifier (AT) and a DPDT relay (RP).  Again, these components interface with the TCW Safety Trim box, the Atkinson pitch trim servo, and the Trio A/P pitch servo for the autotrim feature to operate.

You may note some chicken scratching writing on the wire labels (…at least you do now!). When I added the Triparagon as a Component Wire Location Identifier [N=nose, I=Instrument Panel, H=Hellhole, etc.] I not only changed these wire labels from A (Avionics Bay) to T (Triparagon), but also the end component 2-letter designator on a few items, including both of these autotrim components.  Since this wire label heat shrink is not exactly inexpensive, I made the decision to choose function over form here in an attempt to be both cost effective & pragmatic.  Especially on wire labels that honestly are rarely going to see the light of day once this plane is flying.  To put this in perspective, I’ve already printed almost 100 wire labels and have attached about 2/3rd of those.

Autotrim components - Triparagon Left side

One thing I didn’t show in this post was the unraveling and sorting out of the rats nest of nose gear & AEX wires that sat atop the NG30 cover.   I had zip tied them up to keep them out of the way while figuring out my rudder/brake pedal placement, and it looked like an unsolvable/untraceable mass of wires.  In reality, since I had labeled so many of the wires, after a good 10 min I had it all pretty much figured out and the wires in place, close to their final runs.  So, for the nose gear & AEX power, ground & warning signal wires, I heat-shrinked a bunch of the second labels in place, cut the wires close to their final length and crimped connectors onto a number of them as you can see with the AEX ground wire below that will terminate into the Avionics ground buss (G5).

AEX GND wire terminated for Avionics GND BussI also went ahead and removed a good portion of the outer sheathing to the 3-wire cable coming from the Atkinson pitch trim servo positioning indicator.  The black wire of the group that I labeled and terminated with a FastOn connector will be grounded on the main panel ground buss (G4), while the red & white wires will tie together into one extension wire to feed an input into the GRT HXr to show trim positioning graphically on my EFIS.

Pitch Servo GND wire for Panel GND Buss

I’ll be flying tomorrow, which will of course wipe out a good portion of the build day. Regardless, I’m estimating another 2-3 days to finish up this crazy wiring & Triparagon stuff before I get back onto installing the wheel pants (yes, yes!  I know!  You’ll believe it when you see it… ha!)

 

Chapter 22 – Electrifying Administrivia!

I didn’t get a lot done on the actual build today, although I did get a TON of administrative tasks done for my electrical system.

First off, I’m going to reiterate the emphasis and importance that I place on the electrical system.  Finalizing significant portions of the electrical system may definitely not be as sexy as seeing significant portions of the plane go together, but it in my opinion it is critical for many reasons.  First, if the airplane is an aerodynamic housing for these systems, it makes sense to me to know how these electro-whizzies are going to FIT inside the housing before the housing is completed!  Second, it is infinitely easier to work on fitting those electro-whizzies into place before the housing (eg fuselage, strakes, nose, etc.) is completed.  In addition, it’s nice to be able to track the weight of these components, instruments & avionics to allow for a weight cost-to-benefit analysis of each specific component.  There are at least 2 electrical components (StrikeFinder & fuel vapor sensor) that I’ve eliminated from my system simply because the cost in weight to have these installed is simply too high compared to the operational benefit that they currently provide. Finally, I think it’s critical to know what the current draw is for entire system and each of the primary sub-components of the system.  Obviously it’s impossible to have any current analysis on hand if the decisions on which components will be used haven’t been made. Clearly just dumping a bunch of components together into the ship, even if they are wired up correctly, won’t cut it from a systems standpoint.  For me it’s simple: Better to know all this now AS I construct the airplane rather than later . . . and yes, that’s just my opinion.

Looking forward to after the airplane is flying, with aerodynamics ascertained and airframe structurally integrity verified, then the lion’s share of importance is placed on OPERATING the aircraft.  Operating the aircraft relies on electrical systems, and requires those systems and components be optimized and working correctly.  Of course there will always be a need for fine-tuning these electrical components and a good ability to troubleshoot them as well.  In short: effective & efficient troubleshooting comes down to thorough & meticulous system documentation.  This holds especially true later on down the road when equipment upgrades, swap outs, additions or even removal is wanted or required.

I’ve seen a firsthand example of what a royal PITA it can be when system documentation is not on hand and you’re trying to troubleshoot, understand and/or upgrade your aircraft electrical system components. Specifically on my buddy Marco’s recently acquired already-built Long-EZ.  I spoke with Terry Lamp, the builder of Marco’s Long-EZ, at Rough River about the lack of electrical system documentation.  Terry had created a whole slew of electrical system diagrams & documents for the airplane, but gave it to the new (2nd) owner when the new owner bought the plane.  However, somewhere/somehow the second owner never transferred the electrical system info to owner #3.  Fast forward to Marco as owner #4, and he’s sitting there doing a LOT of head scratching to figure what was done, installed, modified, etc. on the electrical system.  Understandably not Marco’s fault at all, but clearly not a lot of fun.  The bottom line is I plan NOT to be an aircraft owner that doesn’t have an in-depth ability to quickly assess, analyze and identify an electrical system problem due to a lack of good documentation (ala owner #2!).

Ok, with all that said (yes, rant over & off soap box!) . . . I spent quite a few hours today updating my electrical system diagrams & annotating them to reflect what was actually wired on the Triparagon.  In addition, I also deconflicted a number of grounding positions, and consolidated a few ground paths as well.  At times this took digging back through the manuals, and certainly involved cross-referencing and updating a bunch of my different wiring diagrams to ensure they all told the same story.   In addition, I annotated the nearly 50 wire label codes I printed out into my wire label tracking spreadsheet.  Finally, I really can see how finalizing the Triparagon wiring, which I’ll estimate at a good 30% of the overall aircraft wiring, really helps in synching the remaining wiring pinouts, grounds and wiring circuits in playing well together.

Tomorrow I’ll get back to the physical tasks of build, but today was definitely good for keeping my electrical system documentation up to speed.

 

Chapter 22 – Electrical System

Of course at this point my electrical system is analogous with the Triparagon.  Since, that being said, it is true too that the majority of my electrical components are mounted, or will be mounted, on the Triparagon.

After spending a good couple of days here & there populating the Triparagon components with wires to & fro the various parts, and finalizing a large number of circuits for the resident things on the Triparagon, it then stood to reason –and begged the question: Does it work?  Yes, it was truly time to test install this monstrosity.

So I did a mock up install of the wired-up Triparagon onto its mounting tabs in what I call the Avionics Bay (instrument panel to F22) of the Long-EZ.  I also installed the Voltage Regulator to see how it fit into the mix.  Below you can see the left side of the Triparagon & the Voltage Regulator.

Triparagon mock install

And a shot of it from the right.  I’d like to point out that up to this point the Triparagon has definitely met, or exceeded, my design goals.

Triparagon mock install

To give you all a sense of space…. specifically the space NOT taken up by the Triparagon (aka “legroom”) I took a couple of shots from close to straight in line with the edge of the the NG30 plates that house the nose gear motor.  In addition, the nose wheel cover (NB) also provides a “natural” barrier & offers a bit of standoff protection from wayward feet or legs to help keep the Triparagon out of accidental harm’s way.  I would like to point out that the current Triparagon wiring is in the initial “free form” stage and has not been organized, nor secured in place yet.

Triparagon mock installTriparagon mock install

There’s still just a bit of cross-connect wiring that needs to be done on the Triparagon proper, along with some final prep of the mounting tabs and the installation of the top cross shelf before I move back onto installing the wheel pants.

 

 

Chapter 22 – Inching forward . . .

I started off today by taking a pic of the pitch level of the mounted Triparagon.  As you can see, the addition of the last 3 nutplate mounting hard points tilted the Triparagon ever so slightly forward.  Nothing that can’t be reworked or overcome during the installation of the top “shelf,” but it is something for me to take note of to ensure I get 0° level.

Mounted Triparagon Pitch Level

Here’s a shot from the top to show the mounted Triparagon in comparison to the CL.  Again, you can see that the Triparagon is very closely aligned, so not bad.

Mounted Triparagon CL alignment

I cleaned up the left side layups on the Triparagon nutplate mounting tabs.  In the pic below you can see that the top F28 Triparagon mounting tab still needs to be cleaned up.

Trimming left side of Triparagon mounting tabs

I then laid up 2-ply BID layups on the RIGHT side of the Triparagon nutplate mounting tabs.  I then clamped these right side layups so that the glass would cure as flat & tight as possible to allow the Triparagon to mount back into place close to its original installed position.

Glassing right side Triparagon mounting tabs

While the right side Triparagon mounting tabs’ glass cured, I took a few minutes to re-drill the GIB seatbelt crosspiece screw holes, since I had inserted G10 hard points to buttress the square cross tube.

Re-drilling holes in G10 reinforcements

Here’s a closeup shot of the initial drilling of the G10 hard point in the GIB seatbelt crosspiece screw hole.

Re-drilling holes in G10 reinforcements

I then started back working on the actual Triparagon by remounting the electrical components to it.  I also drilled a couple holes to allow a zip tie to be used for mounting the Trio autopilot Autotrim relay –along with a patch of velcro.

Mounting Trio A/P Autotrim system relay

I wired up the G5 avionics ground buss to connect it to the bolt mounting the G4 panel ground buss.  Here’s a shot of the left side Triparagon.

Left side Triparagon

Another shot of the left side Triparagon.  You can see below that I also wired the E-bus to the Schottky diode.

Left side Triparagon

Below is a shot of the electrical components remounted to the right side Triparagon (with a pic hue for some reason).

Right side Triparagon

And another shot of the right side Triparagon.  Again, note that I wired the E-Bus feed by adding a wire between the Main Buss terminal to the Schottky diode (sorry for the slightly blurry pic).

Right side Triparagon

A few hours later I removed the clamped blocks off the Triparagon nutplate mounting points and cleaned up the 2-ply BID layups.

Glassed Triparagon mounting tabs

I also wanted to add a shot of my prop extension back from Sam at Saber Manufacturing.  As you can see, he added in 3/8″ bolt holes and bushings for the Silver Bullet prop on the prop side, and he also added 7/16″ bolt holes in between the 1/2″ holes for mounting the extension to the engine prop flange.

Modified prop extension

From here on out my main focus will be on wheel pants until I get those nearly fully installed.