Chapters 14/19 – Wings to CS Spar

I don’t have pics of today’s progress because it was pretty much all research and coordination.  Although I have been trying to get into the shop to get the wheel pants prepped, I think it’s more important to get the Wings mounted to the CS Spar, then the CS Spar mounted to the fuselage.  Then, finally, the last piece of mounting flight lift surfaces will be mounting the Canard to the fuselage.

I continued to consult the plans and research other builders’ techniques, taking special note of any builders tips and issues they may have encountered.  In addition, I had a good discussion with my local EAA Chapter 186 (Manassas, VA), and my buddies Marco and Mike Beasley.  Mike has finished all the major aircraft structures on his Long-EZ and is in the finishing stage, so he has amazingly valuable insight on how to do this.

The main topic of conversation I had with my EAA folks is in locating a suitable place to mount the wings to CS spar, etc.  They don’t have anything available at this point, so I’m in hunt mode for a good location with enough size that will allow me to complete these next few steps.  One reason why I’m focused on getting this done soonest is that the weather is forecasted to be pretty good here for the next 10 days, so I’d like to get moving of major pieces part done while the WX is cooperating.

Tomorrow I’ll make some more phone calls to find a good build location and should have my plan nearly finalized for these next few steps.

 

The Push Continues . . .

I am very close to starting back on the build, although it is quite amazing to me how much extraneous junk that I’ve had to contend with from selling my other house.  Dealing with this has been the long tent in the pole preventing me from getting back on the build.  And having been in a full-on repair blitz during the time leading up to the house actually closing, I’m just now really get all the tools & materials sorted out, organized, and put back into their proper places.  Additionally, during the last week I have been doing some odd & end stuff on the build, much of it stuff I was never able to really put together before since I didn’t have all the pieces parts in the same location.  As I’ve been getting my shop and house in order to build, I’ve also been focused on prepping –at least mentally & planning wise– for some other parts of the build. So, here we go.

Canopy Latch: A note that I’ve had for a while in the middle of my electrical switch diagram states to account for the panel space required by the canopy latch arm that sticks out horizontally into the space near the throttle handle.  I became acutely aware of how much space the canopy latch was really taking up when I sat in my buddy Marco’s Long-EZ specifically to note clearances, required reach to cockpit items/switches, and simple ergonomics.  It emphasized that the note on my switch diagram truly had merit, and that I must indeed account for this most necessary but intrusive component.

Thus, back at my hacienda, I finally got around to pulling out the EZ-Rotary Canopy Latch kit that I bought from Jack Wilhelmson (eznoselift.com).  I first (re-)inventoried all the parts to ensure I hadn’t lost anything over the years.  I then did a quick (re-)review of the installation procedures to get a feel of what I was up against.   My main current concern was of course the clearance with the instrument panel, and luckily with this setup the bearing block hangs down from underneath the longeron, and not straight out from the panel, thus giving me back the 3-4 square inches that I wouldn’t have been able to use on my instrument panel if I had installed the plans version of the canopy latch (pic below is from Jack’s website).

EZ-Rotary Canopy Latch

Electrical System:  Ah, yes, this beast keeps rearing its head.  Yes, yes, I am very close to a final system configuration, at least for now.  But stuff is still cropping up!  I equate it to trying to get all the dish soap out of a sponge: every time you squeeze it more soap comes out again!  So . . .

Pitot Tube Electronics & Components: Starting back in the beginning of 2013, my buddy Marco and I started brainstorming on a heated pitot tube design for our Long-EZs. Recently, Marco has been doing some truly amazing work on the electronics that drives the pitot tube heat.  In preparation for the electrical components that he’s developed for the pitot tube, I recently purchased another airspeed switch, and a new 3-position ON/OFF switch that has a momentary ON position in the farthest up point to reset the electronics if need be.  Marco has been detailing a lot of this on his phenomenal blog, What have I gotten myself into!

Control Stick Button Role Refinement & Swap: While down in Virginia Beach getting my first Long-EZ ride from my Marco, he at one point recommended that I swap my alarm momentary shutoff (left side of stick) with my A/P disengage & Pilot Controlled Steering (PCS) button (upper right of stick) on my control stick.  Well, I have to admit that I was a little resistant at first, but after pondering the idea and getting into the Trio Avionics Autopilot manual (and really finding out the advantages of using PCS), I actually had an epiphany while driving home one evening: since the top right button is the hardest to reach on the stick, then why not use it to control something that I will use very occasionally in the air, and almost exclusively on the ground.  Whereas with my new found understanding of PCS, I am confident that I will use that much more while flying.  Thus, I wanted the A/P button in a much more user friendly place on the stick, so of course I swapped them… which is simply code for I changed the CAD drawings for both the buttons’ electrical wiring connections.  Nonetheless, thanks again Marco for setting me straight!  ha!

Here’s a pic identifying my current Infinity control stick button & switch assignments.

Infinity Stick Switch Assignments

AG6 Warning Annunciator (#2): As I was getting a bunch of these ‘final’ items squared away before jumping headlong back into my build, I submitted parts orders with B&C, Mouser & Aircraft Spruce.  Part of my order with Mouser was a direct result of my discussion with Rich from AircraftExtras.com, who gave me a bunch of great info on the AG6 warning annunciator.  To drive a myriad of warnings that would normally require an LED on the panel, I ended up calling a number of vendors to confirm the correct resistor values & wiring circuitry to use with their specific products.  Once I had the recommended resistor values in hand, I fired off an order to Mouser for all of them.  That also helped me to finalize which of my components would/could utilize the AG6 to annunciate an alarm condition.  One thing was certainly clear after I figured out what-was-going-where for my alarm annunciations, and that was that I didn’t have enough “where” to go to!  I needed another AG6 to handle the increased number of components connected to the AG6(s) to annunciate their alarm conditions, so I ordered a second one.

AG6 Warning Annunciator

The missing 2-Amp Circuit Breaker!  One day last week as I was updating my electrical system diagrams I ran across the 2-Amp inline fuse for the SD-8 backup alternator activation switch on the circuit diagram.  As I was assessing that switch specifically, for some reason the inline fuse didn’t seam like the right fit.  I pulled up the B&C install manual and sure enough it showed a 2-Amp circuit breaker, NOT an inline fuse! I then went back through the last couple of versions of Bob Nuckoll’s Z-13/8 system architecture diagrams and…NO inline fuse!  “Huh?!” sez I, “Where did I get the idea for placing a 2-amp inline fuse there?”  Well, I finally found it in an old version of the system diagram that I had started with back in 2012! I guess it pays to review, or, well, it actually costs money since I had shell out some more to buy a 2-Amp Circuit Breaker.  Regardless, I’m just glad I found my oversight & corrected it ‘early’ on.  By the way, this scenario is exactly why I’ve been critically assessing literally every component in my electrical system!

Engine Cowling Installation:  Over the past few days I also wanted to get a lot smarter on exactly how the upper & lower engine cowlings would be mounted, specifically the hardware to do so.  This meant getting much smarter on Camlocs and the Skybolt Croc system.  I researched a fair bit and bought a few basic Camloc components in my last Aircraft Spruce order to test them out. In addition, I’ll be using Mike Melvill’s 82° stainless steel hex-drive screws that he discussed in the Canard Pusher newsletter (CP 73).

Skybolt Adjustable Receptacles

Electrical & Aircraft Component Weight:  Upon receiving the new 2 amp circuit breaker and AG6 warning annunciator I decided it was time to spend a good hour to update my estimated aircraft weight worksheet.  I added all the new components, eliminated old ones, and weighed a number of components that until previously I only had factory listed or estimated placeholders for.  When I finished, my Long-EZ had gained 10 lbs, with its new estimated weight still just under my max goal weight of 1,000 lbs… but just barely! And by barely I mean less than a pound under.  The good news is that I have a lot better idea of what is going into my airplane and now have hard weight data vs. estimated/unknown data variables.  Obviously, since I now have a lot of this stuff on hand, I can get the actual weight of each item.  Moreover, I have padding built into the weigh figures for the electrical system, avionics/equipment, and main airframe components.  Thus, I suspect to be somewhere near 1,000 lbs. for my final weight, ± about 30 lbs. (yes, yes, more likely plus than minus!)

Integrated Backup Battery System (IBBS) model selection:  One thing that I did in the planning of my future components order is to mock up the fit of my TCW Technologies IBBS in the nose where I plan to install it.  After a discussion with Marco on the W&B on his new Long-EZ, I figured a pound of extra weight gained by moving up from the 3 amp hour IBBS unit to the 6 amp hour unit would actually be beneficially.  However, there’s just one problem with moving up to the bigger 6 AH IBBS unit: it won’t fit in my planned location!  No worries though since the original 3AH IBBS unit that I had initially decided on will work, so back to square one.  Another decision crossed off the to-do list.

Fuselage Trueness, Squareness & Alignment:  At some point after returning back from overseas I took a myriad of different measurements on my fuselage, from a myriad of different locations on the fuselage: bulkheads, Left/Right/Center, angled, etc. to assess & evaluate to what extent my fuselage is true, square and aligned.  If you’ve read much of my blog you know that my fuselage is not perfectly aligned.  That being said however, I had never taken the time to really sit down and figure out what my measurements meant. After really pouring over them for about 15 min, I concluded that my fuselage is acceptably square between the firewall and F22 bulkhead.  Another thing I did when I made my measurements was to clamp a 6 foot level to the front & aft sides of my fuselage and then measure the outboard distance between each straight edge/level.  What I came up with after multiple measurements, and after recently analyzing the data, is that the difference between each side (at essentially B.L. 36L & B.L. 36R) is just a hair over 1/8″ off.  Not bad, and easily correctable when I install the CS spar & canard to the fuselage, respectively.

Engine Mount Extrusions installation:  This next thing I did was something that solved a question that has been gnawing at me for some time: How exactly will my engine mount extrusions be mounted to the fuselage/CS spar/longerons?  Well, between last night and today I finally measured all the critical players and worked out an installation solution. Since my aft upper & lower longerons are thicker (since I was originally planning on having a much wider fuselage all the way back including the firewall) AND my back seat is about 0.8″ wider, I needed to detail out exactly how thick the extrusions needed to be, and how many plies of BID to use to get the spacing correct.  As you can see, on the lower mounts I’m adding 6 more plies of BID along the sides and using a 3/16″ thick 2024 angled aluminum extrusion.  On the top I’ll be using 1/8″ thick 4130 steel extrusions with 4 extra plies of BID on the sides of the extrusions.  The weight penalty for all this is about 1.5 lbs.

Engine Mount Extrusions

Finally, in prep for my upcoming reintegration back into the build, I performed the ceremonious refilling of the Flox and Micro containers.  And cleaned my respirator masks.  (Hey, if this isn’t a clear indication of getting on with the build, I don’t know what is . . . ha!)

Cleaning respirators

 

My first Long-EZ ride!

Yes, it may sound a little crazy or unbelievable, but I have been building my Long-EZ for over 5 years now and have never actually flown in one until this past week!  The timing actually worked out in the grand scheme of things.  If tried a bit last year at Rough River to get a ride but never actually did.  When my buddy Marco bought his Terry Lamb-built Long-EZ a couple of months ago (a beautiful airplane), he had to A) learn to fly it, then B) fly off 10 hours before he could fly passengers in it, thus satisfying the insurance companies demands.  Last Sunday (7 Aug) he finished his 10 hours, and due to both our schedules, the only time I could fly with him in the near future was Monday, 8 August.  So I scooted down to Marco’s Sunday evening, we flew Monday, then I returned back to the DC area Tuesday.  I headed straight to the airport to pick up yet another out-of-town visitor!

I have to say that while flying the Long-EZ for the first time was a blast (albeit from the back seat), it was also a bit anti-climatic.  The tales and yarns of how difficult and unique this bird is to fly seem to be a bit over-dramatized and exaggerated, and I’m not sure why. This plane is a pleasure to fly and it handles very well.  Of course, the overarching impact of my personal historic first Long-EZ flight is that I am incredibly motivated to get my bird built and in the sky!

I hope you enjoy the video!  Cheers.

Chapter 22 – Why Vic?! . . . Why???

It’s funny to me how I can ponder on something for a fair amount of time and then as if by putting mental energy into a concept, it reveals itself in a some what short amount of time. As with many things lately, certain discussions have fostered various thoughts about various instruments, avionics and switches on my panel.  Yet another discussion I had with Marco about his recently purchased Long-EZ –which incidentally has proven to be quite the test bed in that the handful of discussions that we’ve had concerning his new bird have spawned a number of viable system designs mods in mine– and the comment that he made on wanting to have a Garmin-free bird (due to their high prices on data updates), got me to thinking a bit . . .  but admittedly, with everything that’s been going on lately, I really wasn’t thinking that much on it!

What I had been thinking about for some time was having a GPS with a decently larger screen size than the GTN650, but one that would still fit comfortably in my panel.  In fact, I was thinking about this even more after I learned that GRT had debuted (FINALLY!) the 8.4-inch HXr at this year’s SNF.

Well, not sure if you got a chance to read Vic Syracuse’s article on the Avidyne IFD540 GPS Navigator in the August 2016 edition of Kitplanes Magazine.  All I can say after doing a bit of research for the last 3 days on this puppy is WOW!  This guy is packed with a ton of features, and in addition, its screen size falls right in between the GTN650 and the GTN750, so it looks like it will really work well for my panel size.

Avidyne IFD540 GPS Navigator

Moreover, the Avidyne IFD540 is a drop in replacement for the Garmin GNS430, so the pinouts are nearly the same as it is with all Garmin GPSs.  I spent about a half hour confirming and updating all the component crosslink pins to ensure that this would work in my electrical system’s wiring schema, and it does!  I had to change the actual pin ID numbers on about 70% of the pins (the D-Sub connectors identifying numbers are different as well), but did the swap in my wiring diagrams in short order.

And yes, I did say last week that I was done with my electrical system planning for the time being, but apparently this is the nature of the beast in building a homebuilt experimental airplane.   So again, I think I’m done in having finished my electrical system planning (at least for now!).

Chapter 22 – A few Yays & an Oops!

Over the past few days I’ve pretty much finalized all I can with my electrical system planning at this time.  I would hazard a guess that over the past couple of months I’ve moved the “finish” dial on my electrical system design & documentation from the 89-93% range to the 96-97% complete range.  There are still a few more admin things I need to finish, and depending on any future changes in vendor-mandated installation requirements on my respective components, I’ve pretty much got the design dialed in to the point where I can implement the electrical system plan where permitted from here on out as I build.  I do have a couple of switchology decisions to make, but those won’t come until I mock up the panel and play around in a simulator-type setting while making airplane noises.

Moreover, I met another design milestone by creating wiring diagram 13 showing all the wiring for the 6 throttle handle-mounted switches.  Since I’m making the throttle handle removable I’ll be running all the wires through a 24-pin AMP CPC connector–the same style connector that I used on the nose gear actuator connectors where I swapped out the stock Molex connectors.  On the throttle handle I’ll be wiring all the switches with new wiring and swapping out the old stock circular Amphenol Mil-Spec connector with the much lighter and cheaper TE Connectivity AMP CPC connectors.

24-pin AMP CPC connector vs old

After removing all the existing electrical potting material and then stripping all the throttle handle switches of the myriad of resistors and capacitors, which created a near-impenetrable labyrinth around the back side of each switch, I was able to tone all the switches out.  I was pleasantly surprised to find that I had mistakenly ID’d the bottom toggle switch as a SPST switch rather than the DPDT switch that it actually is.  I had already targeted an $80 OTTO replacement switch for this position, but after this latest round of investigation I can belay that order and use the stock switch for my Landing Brake!

With my throttle switches clearly identified, and the wiring to & from each switch, I could then marry up my initial throttle switch diagram with the 24-pin AMP CPC connector and finalize the throttle handle’s P4 connector pinout diagram.  I have all my multi-pin circular connectors detailed in a PowerPoint slide deck (it just evolved that way).  And since I currently have seven connectors on the aircraft (P1-P7), I obviously need a diagram for each connector.  Unfortunately, I hadn’t created all the diagrams, so down another rabbit hole I went for a couple of hours to finish all the templates for all the circular connector pinout diagrams, as you can see in the pic below.

P1-P7 Connector Pinout Sheets

Now, each connector pair gets 2 pages detailing the pin assignments.  The first page (top of the 3 pages in the pic below) details the general information about each connector: number of pins, part numbers, mounting flange (if present), hole number schema, pins, sockets, and standard vs reverse sex connector.  The second/back page (middle & bottom in pic below, with bottom page info populated) shows the detailed pinout for each connector side, with wire colors and wire function/connectivity.  I of course finalized populating all this information for each side of the P4 throttle handle switches connector.

AMP CPC pinout diagrams

As for wiring diagram 13 depicting the wiring for all the 6 throttle handle-mounted switches, below top you can see the initial draft versus draft #3 in the second pic below.

Throttle Handle Switches

Throttle Handle Switch Wiring via P4

I knew that the top left throttle handle switch that was clearly designed for a specific F-15 system was not going to work for my application.  This switch is nearly heavier than all the other switches combined and in my estimation is probably a good 30% of the stock weight of the throttle handle as it was shipped to me.  I pulled this switch and then spent a fair amount of time identifying its replacement.

Removed F-15 throttle handle switch

And here’s what I came up with: the OTTO T5 mini trim switch.  The more complete description is a commercial grade 4-way plus center pushbutton trim switch.  The pic below is a stock photo off the Mouser website.  In actuality, the switch I ordered does have the “stadium” grips on the top as this pic shows, but it differs in that my switch is gray and it is press fit vs. threaded mounting.  If you’re curious about the switch assignments, here they are:

  1. UP – Trio Autopilot Fuel Information Screen Cycle
  2. DOWN – AFP30 Air Fuel Data Computer Screen Cycle
  3. LEFT – GRT HXr EFIS Page Flip
  4. RIGHT – Garmin GTN650 NAV Source Select
  5. CENTER – Garmin GTN650 CDI Source Select

OTTO T5 Mini Trim Switch

As for the other Throttle Handle Switches, here’s the layout:

#1 – Outboard Front – 5-Position Mini Switch (described above)
#2 – Inboard Front – COM PTT
#3 – Inboard Side Top – COM1 Freq Flip-Flop
#4 – Inboard Side 2nd Down – Nose Gear UP/DN
#5 – Inboard Side 3rd Down – A. Remote Start Arm   B. Trig TT22 XPDR Ident
#6 – Inboard Side Bottom – Landing Brake UP/DN

Throttle Handle Switches

Alright, moving on!

As I was reviewing the P-connectors pinout diagrams, I set about to confirm some info on my P3 (Trio autopilot pitch servo) & P7 (Trio autopilot roll servo) connectors.  For some reason our good friends building non-TSO’d products for our birds typically use auto grade Molex connectors.  Being a true disciple of Bob Nuckolls, and having had other discussions with some smart bubbas on this topic, I am simply (and clearly) not a fan of Molex connectors.  Especially for the autopilot roll servo which will be located on the back of the center section spar in the engine compartment.  I want more environmental protection for this connector.  So, my dear friends, I was confirming the wire colors and pinouts on the P7 connector with the Trio install manual–since I had just ordered a reverse sex 4-pin sealed connector (so that it was physically impossible to connect up either servo in the wrong spot) on my last Mouser order– AND that’s when a disturbing question popped up concerning both the P3 connector, and the pitch servo.

You see, I had incorrectly ordered a 4-pin connector for the pitch servo in my haste to get all the required electrical pieces parts in hand.  It didn’t require any O-ring seals since it was in the avionics bay, so I simply pulled the trigger.  But while reviewing the Trio autopilot installation manual wiring diagram, I realized I had forgotten about the 2 extra wires coming from the pitch servo for the Auto Trim feature.  But why had I forgotten these wires?  I then pulled the pitch servo out and –what?!– only 4 wires!  Hmmm, maybe they were tucked inside the servo since this was an “optional” (key word here folks) feature.  I pulled the cover off the servo, and no joy.  There was not an extra pair of wires or connection points inside this servo.  Ok, what’s going on here?

I went to Trio’s website, and I still got the impression that the Auto Trim feature was a standard feature of Trio’s Gold Standard servos and merely labeled as “optional” since the builder had to add a relay, bridge rectifier and wire it all up for it to work.

Trio Autopilot Pitch Servo

I called Chuck at Trio to ask him about this latest puzzling revelation.  He and the Trio gang were just getting ready to head out the door to Oshkosh, but he took the time to have a detailed conversation on the status of my pitch servo.  So here’s the deal: A few years ago the Auto Trim feature was an actual priced option for the Trio Gold Standard servo. However, they decided to simplify production and simply make the Auto Trim a standard feature on the pitch servo, yet still optional as to if the builder/owner wanted to utilize it or not.  Since this was my impression all along, it never entered my brain as a data point when I bought these servos from a fellow homebuilder (Rans S7 I believe) off of Ebay.  If you recall, I had the servos sent straight to Trio who made one engineering upgrade, ops checked the servos and then sent them on to me with the install kit required for a Long-EZ. All was good!  Or, so I thought.  Hmmm…

Trio Autopilot Pitch Servo

Okay, lesson learned!  The money I saved on buying these servos off of Ebay has been reduced to virtually nil now that I’ll be sending the pitch servo back to Chuck, along with a couple hundred bucks, to have the Auto Trim feature installed.  All in all, no big deal.  I’m just glad I caught it early on.  And I guess technically this was two Oops since I also had to spend $10 to include all the pieces to make up a 7-pin AMP CPC connector on my last Mouser order!  [Note: I’m using a 7-pin connector since they don’t make a 6-pin.]

In closing, I currently have everything either on hand or on order for my electrical system. As I did a couple of years ago, I’ve included a rundown below of all my electrical system diagrams (wire book) up to this point.  As you can see, I have a few more systems to figure out, but nearly all of the really critical stuff is complete.  As for the Main, Battery and E- Busses, I won’t diagram those out until all my other system designs are completed and installed.

0. Index Page
Z.  Z-13/8 Electrical System
A.  Switches, Circuit Breakers & LEDs
.99 Grounding Busses
1.  Panel Components
2.  Radio & audio system
3.  Panel Power
4.  Electrical System Components Location Diagram
5.  Aircraft Wire Labeling Sectors Diagram
6.  Nose Gear
7.  Pitch & Roll Trim Systems
8.  Lights: LDG, TAXI, NAV, STROBE
9.  Engine Info Management
10. Fuel System
11. Cockpit Lighting
12. Landing Brake
13. Throttle Handle Switches
14. Control Stick Switches
15. Integrated Backup Battery System & X-Bus
16. Alarm & Warning Systems
17. Charging System
18. AG6 Warning Annunciators
19. Electronic Ignition
20. P-Mag Ignition
21. Heater System
22. Starting System
23. ELT
24. Heated Pitot Tube
25. Trio Autopilot
27. Main Bus
28. Battery Bus
29. E-Bus
30. Long Wire Runs

This wraps it up currently for my electrical system design and planning.  From here I’m going into house cleaning mode (multiple out of town visitors arrived and/or arriving!) and shop cleaning & organization to move forward on the actual build…  woo-hoo!

 

Chapter 9 – Gear fairing tops glassed

As I mentioned in my project update, I decided that I needed to flip the fuselage right side up to glass the top sides of the gear fairing.  I hadn’t planned on flipping the fuselage for quite a while, but plans change when one (read: ME) fails to account for issues such as the heat shields blocking access to the lower outboard gear leg thus preventing glassing the topside gear fairing if the wheels are mounted.  Sequencing is key in my opinion for optimizing the build schedule, but in this case there was no way around it: the fuselage was going to have to get flipped back upright.

No big deal of course.  I did re-wicker my build steps though to account for the fuselage being right side up.  The plan now is to glass the top of the gear fairings, then do a final check & possible tweak of the toe-in, and then mount the wheels/tires/axles/brakes/heat shield.  With the wheels in place, and the fuselage upright, I can then mount the wheel pants and be finished with all things gear related except for finalizing the brake line install.  As for the stainless steel brake line install, the new timeline works out fine since my stainless steel capable flaring tool won’t be here for another couple weeks.

So I started off today by trimming the TE of both the right & left gear fairings.

Gear fairing TE marked for trimGear fairing TE marked for trim

Once I got the gear fairing TE squared away, I needed to flip the fuselage.  I did about 10 minutes of head scratching before I finally remembered that I had designed the fuselage dolly so that it could match up height-wise with my portable fold out table.  I set the table as you can see below and it matched up great after I set a couple 2x4s with cardboard protectors in place to get the heights equal & matched.

Flipping fuselage

I then very carefully & slowly tipped over the fuselage onto the foldout table using the gear legs as a lever.

Flipping fuselage

Here’s a shot from the inside cockpit side… something I haven’t seen in while.

Flipping fuselage

I then slid the fuselage sideways back onto the fuselage dolly.

Flipping fuselageFlipping fuselage

And then flipped the fuselage right side up back onto the fold out table, and then once again slide it over onto the fuselage dolly.  Once I had it blocked correctly underneath, I then reattached the securing straps.

Fuselage flipped

Another shot of the flipped fuselage from the aft end.

Fuselage flipped

Clearly the bottom side of the gear is close to the ground, someplace that I don’t want to spend a lot of time messing around trying to layup glass.  Luckily my fuselage dolly elevates!

Interestingly, with the amount of weight that my fuselage is packing on, my drill couldn’t handle the torque of getting the dolly platform to raise.  Actually, I should say that my hand couldn’t handle the torque of the drill wanting to rip out of my hand.  So I grabbed a ratchet speed handle and raised the platform its first few inches manually before switching to the drill. [I guess this demonstrates the torque required on the nose gear that Jack discusses in his instructions: to have the gear up at least a foot before climbing in & having it raise passengers from the flat deck position.]

As you can see, I raised the platform its full height giving me (and thus my back!) a much better working height for glassing the top side of the gear fairings.

Fuselage raised up in the airWith the gear height at an acceptable working height, I then marked the right gear fairing a half inch (0.5″) forward of the TE.  This will allow for a good top fairing glass to lower fairing glass bond.

Right side fairing TE marked for trim

I used a razor knife to remove the foam, and then the Dremel Tool to remove the micro that had oozed out the aft end of the foam piece junctions.  I also cleaned the dead foam & micro off the freshly exposed TE lip.

Right side fairing TE trimmed 0.5"

Then came the not so fun step.  For some weird reason the “2-piece clamping method” that I used on the right side fairing didn’t work so well.  I could run my hand up & down the outer surface of the right fairing and depress the foam inwards towards the original gear.  Clearly there were a fair number of air gaps between the applied micro layer and the foam fairing pieces on the right side fairing.

With the size of the air pockets the practical solution was far beyond injecting epoxy or anything else under the foam pieces, I was going to have do a sort of rebuild on this fairing.

Right side fairing unattached foam removed

Enter X-30 Expanding Foam.  I know a lot of builders have used this foam for a variety of things, but I personally haven’t used it before.

X-30 Expanding Foam

After reading the directions I decided that I would heed the warning of so many builders before me that this stuff really does expand 30 times its initial volume.  With this in mind I marked equal pencil lines in 2 small cups less than an inch up for parts A & B of the X-30 foam.

Part A & B cups marked for foam

I poured the part A & the part B X-30 foam in the separate small cups, and then as per instructions mixed them in the larger cup.

Ready to roll with expanding foam

For those not familiar with the X-30 Expanding Foam, it has a 15-20 second mix time before its immediately poured and/or applied to the surface.  I didn’t set up any dams or anything since I applied it straight to the surface of the right gear fairing.

Expanding foam applied to right side fairing

Here’s a wide angle shot of the right gear faring with the expanding pour foam applied to it.

Expanding foam applied to right side fairing

While I let the expanding foam cure some I went to work on the TE of the left gear fairing.  As with the right gear fairing I trimmed the foam 0.5″ from the TE.

Left gear fairing TE marked for trim

Left gear fairing TE 0.5" trimmed

After finishing trimming the TE on the left side, I turned my sights back onto the right side gear fairing.  I started out using the Stanley Surfoam grater to trim the foam down (left pic) and then used my sanding board to finalize the foam sanding (right pic).

Right gear fairing foam rough shaped

Right gear fairing foam sanded to shape

I then cut another 4 pieces of UNI off the roll.  This time around I added a half inch to make the width 11-1/2″ wide vs the underside 11″ wide.  I cut the UNI at a 30° angle across the entire roll.

I then mixed up some flox and applied it to the left top gear fairing foam & glass junctions at both the LE & TE.  I then micro’d the surface of foam gear fairing before laying up 2 plies of UNI oriented in opposite 30° angles.  I overlapped the 2 plies of UNI onto the bottom fairing glass by about 1.5″ the entire length of the LE.

Right top gear fairing glassed

A front shot of the glassed topside left gear fairing.

Right top gear fairing glassed

With the right gear fairing glassed I then sanded down the blue foam & cleaned up the micro on the left fairing with the Dremel tool.  Once the fairing surface was prepped, I micro’d the top left gear fairing.

Left gear fairing trimmed & sanded

Left top gear fairing glassed

I then laid up 2 plies of UNI at opposite 30° bias just as I did on the right side gear fairing.

Left top gear fairing glassed

Left top gear fairing glassed

After laying up the UNI on the fairing I ensured that it was trimmed on both sides.  I also peel plied the UNI overlap onto the lower fairing glass on each side.

Right & Left top gear fairings glassed

Since I used MGS 335 with slow hardener, I have a few hours before I’ll razor cut the overhanging glass.  When the layup gets to that green point I’ll also apply dry micro to the depression along the TE.

Once I get the gear fairing cleaned up I’ll confirm the toe-in as I mentioned above.

 

 

Chapter 9 – Main Gear Install Plan

Today I didn’t make it to the shop to do any actual physical work.

I did however spend a good 7 hours planning and sequencing out the remainder of my Long-EZ build.  Specifically, I spent the majority of time creating my build plan & task list for installing the main gear, axles, wheel & brake assemblies, tubes & tires, dealing with toe-in, glassing the gear fairing, identifying required tools, hardware & materials, and the eventual install of the wheel pants, as well as well as a myriad of other associated main gear related tasks.

To finalize this plan I reviewed the plans Chapter 9, Canard Pusher plans changes, Matco wheel/brake install manual, Eureka CNC gear fairing install instructions, CSA articles, Sam James’ wheel pants install manual, builders’ websites, forums, and my compilation of main gear related build notes over the years.

Since I now have the lion’s share (about 90%) of the specific main gear install plan in hand, I can go back to finishing up nose & elevator stuff as I start transitioning into focusing on the main gear final install.

 

Chapter 13 & 22 – This & that

I started out today actually spending some time finishing the blog post from yesterday.  Clearly I’ve been a little busy on the plane build so it can be a challenge sometimes getting a bunch of work done and then keeping the build log updated.

Due to the holidays and some work stuff I got a late start today.  As I mentioned in last night’s tome, I’m compiling another few orders for ACS, Stein, etc. and I’ve been doing a bit of digging to make sure those are complete as possible before I pull the trigger.

One item I worked on earlier was developing the order for my PC680 battery strap.  Since this will be custom made, I’m making sure that all the dimensions are absolutely correct.  I’ll probably pull the trigger on that order tomorrow or just after Christmas.

After dinner, I putted around looking for a piece of foam to act as a mounting pad for the battery buss and the relay that drive the E-Bus (Essential Bus) during an emergency if the main alternator fails.  The E-Bus will be driven by my 10 Amp back-up alternator, B&C’s SD-8, but if the main bus goes berserk, than a couple of switches need to be flipped to shut down & bypass the main buss & fire up the E-buss.  The relay that I’m mounting here is controlled by one of those switches.

I found a piece of 3/8″ scrap Divinycell with 1-ply of BID already laid up on it, and since I’m only laying up 1-ply of BID anyway, the other bit of cured BID is fine with me.  This is actually scrap from the big 3/8″ thick panel I did back in Germany that my side consoles & arm rests were cut from.  For this pad, I wanted 3/8″ thick vs 1/4″ thick foam so that the nutplates would have enough clearance.

Scrap foam for Battery Buss Pad

Ahh, speaking of nutplates, here they are now!  All 6 of those suckers… that I just made up tonight.  Actually, I’m getting pretty good at cranking those guys out and can gin one up now in just a few minutes.

The 4 nutplates on the bottom of the bus & relay mounting pad are the K1000-08’s, and the 2 on the top are the K1000-06’s.

"Ahh, nutplate city limits . . . "

And here’s a shot of the front of the Battery Buss and Relay mounting pad.  You may be wondering why I’m even going with this mounting pad vs just mounting these to the back of Napster (aka F1-3 Bulkhead).  Well, I just didn’t care for the idea of putting 6 holes, albeit small, into a primary structural bulkhead.  So I opted for this solution to minimize holes in Napster.  (I’m sure once you see the holes for all the wires, you’ll ask, “Who is he kidding?!”  ha!)

As you can see, I also beveled the edges to provide a nice ramp for the BID.

Front face of Batt Bus & relay mount pad

I dug around in my scrap BID pile but couldn’t find anything big enough to cover this piece.  Pickings are getting sparse in the BID pile!  I had to head to my local Glass Cutting Table and cut me a fresh slice off the rack!

I then put the BID in its pre-layup home: plastic, since ALL layups are prepregged . . . aren’t they?!  haha!  I traced about a 1″ space from the edge of the mounting pad onto the prepreg plastic to ensure that there would be a decent sized overlap for the BID onto the surrounding glass once the pad is attached to Napster.

Figuring out BID prepreg for layup

After filling the nutplates with plastic wrap to protect the threads and micro’ing them all into place with blue wing foam backers, I then proceeded to mount the pad.  In my new found love affair with 5-min glue, I actually left 3 small spots open on the back of this pad with no micro-paste in order to place dabs of 5-min glue.  I then pressed it onto the aft right side of Napster and held it in place for about 5 minutes.

I then cleaned up the edges, made sure the fillets were good and that the edge ramp foam was micro’d as well.  I then cut my prepregged ply of BID on the previous outline that I had drew and laid it up.  Here it is below with the outer piece of plastic still in place.

I should note that I realized a tactical error that I made just before I laid up the BID.  I looked at the pad, then grabbed my battery buss fuse block and held it in place where it would mount.  As I suspected, the access to the Fast-On tabs on the left side near the NG30 upright would be a little tight, albeit not anywheres impossible, to get the wires’ Fast-On connectors on & off… not that I’ll be doing that a lot once the electrogizmos are set.  But, just to add a little ease of access, I skooched the whole thing over to the right about 0.2″ and filled in the resulting gap with more thick micro.

Prepregged 1-ply BID laid up

I then pulled the prepreg plastic and proceeded to form the sides down into place.  I noted that for some reason at the upper right angled corner that the BID had split open and it wasn’t allowing me to coax it back to being somewhat normal.  With that corner being thin, I grabbed another piece of scrap BID and laid it up over the small corner split and pressed on.

After the BID was all wetted out and the lay down looked good, I peel plied the layup with one piece of peel ply cut at the corners so that it would lay down over the irregular surfaces.

One last note.  After I had pulled the mounting pad away from the NG30 upright almost a 1/4 of an inch, I noted after a bit of time laying up the glass that the darn thing must have moved some on me, mainly at the top, but it did move back towards the center a bit.

Oh, well.  No real harm . . . no foul.

Pad installed w/ 1-ply BID

I was also going to micro in the H100 foam in the center space between the BC1s for the front bulkhead, but as I was prepping to do so, my Spidey sense started tingling stating that I should wait until I clear up a few more variables surrounding the battery compartment components.  So, I waited.

Tomorrow I’m planning on putting the NG30 area back together after cleaning up the front battery buss layup and drilling all the Saran wrap out of the holes.  I also plan to get the spare tire figured out, the brake reservoirs and associated Click Bonds glassed in place, and the front nose foam cut and ready to glass into the battery compartment area between Napster and the F-7.75 bulkhead (which I’ve nicknamed “the Roundel”).

 

 

Chapter 13 – Hittin’ the brakes!

Funny, if you look at all the pics in this post you’d swear today was all about brakes, which I definitely hit some significant milestones with today.  In actuality, today was almost entirely spent on, you guessed it, the electrical system, but I’ll get into that in a minute.

I received my 3/16″ Statoflex 124 brake line hose assemblies today and they’re exactly what I wanted!

Stratoflex Brake Hoses

Here are a couple more shots.

Stratoflex Brake HosesStratoflex Brake Hoses

If Bob Nuckolls is the King of Electrons, then I’d say Tony Bingelis was the King of Engines, and almost all things mechanically related to aircraft.  Now, just as I have on occasion angered the gods, mainly Burt, (as if he actually knows what I’m doing… ha!) by violating his edicts with a few mods here & there, so too did I violate one of Tony’s.  Tony states to always go with new hoses and not NOS (New Old Stock), but given the history of these hoses, the care in which they were stored (detailed), the price compared to new, and the fact that they were EXACTLY what I was looking for dimensions & fittings wise, I just couldn’t pass them up.

Below is a shot confirming that the new hoses work with the AN3 fittings I have on hand. Sweet!

Checking AN3 fitting fit . . . it fits!

Continuing on with the brake theme, I spent the latter part of the evening working on my brake lines in the forward NG30 nose area.  I cleaned up the inevitable flox globs that formed on the edge of my threads just over the blue tape to offer me a really good challenge of removing 1/2″ pieces of blue painting tape.  (Maybe this is how the angered airplane guru gods get me back, by making even the smallest tasks a total PITA . . . haha!)

I know that my brake line system may seem a bit robust, or entailed, for what it’s actually accomplishing, but I didn’t want to just go the EZ way out and throw in a couple of runs of Nylaflow and call it a day (I’ll do that for the rest of the nose brake lines!).  Remember, the components making up these lines are literally the smallest you can get in every category: 1/8″ aluminum tubing, -2 fittings and -2 Adel clamps.  We’re talking mere ounces, including the diminutive mini-bulkheads, in weight penalty… I’d seriously guesstimate maybe 2 ounces over using Nylaflow/Nylon brake tubings from the main brake line to the Parking Brake Valve (PBV).

Plus it was fun, I learned a lot, and the tubing reminds me of a German brewery . . . Ah, beer!

Nose brake lines in!

Here’s a shot from the other side.  The half loops in the line are simply that, a service “loop” in case I need to rework the brake line.  Since the majority of it is embedded, I wanted to leave enough exposed that I could whittle down in making new flares, etc, if need be.  The aluminum tubing is softer, and bends quite readily, so there was no torquing or strain on the line in making those seemingly tight bends.

As I’m sure you’ve noted, I placed the Parking Brake Valve near it’s final mounting location to check how it fit into the schema.  So far so good.

Nose brake lines in!

Now, onto how I really spent my time.

When I was brushing up on brake line fittings, tubing, flaring and the like in Tony Bengelis’ books, Firewall Forward, and Tony Bengelis on Engines, I noted that he noted that there seems to be a number of “insignificant” things (my paraphrasing) that we overlook in the build until we get to them.  Probably natural, and perhaps less costly in the long run since far less money is wasted on buying things based on future prognostications.

Tony was speaking mainly about hoses, and how builders tend not to give them care until they’re at the point in the build where they need them, and then they most likely have to get them constructed.  Time not building, and perhaps added costs in getting them shipped faster. IMO, there are quite a few areas in a Long-EZ build where this occurs, ESPECIALLY considering that Long-EZs are both plans built and continue to evolve in major sub-systems design due to the open source type metamorphosis that continues with this aircraft.  A few cases in point from the original plans:  Jack Wilhelmson EZNoseLift, Ken Miller’s forward rudder/brake pedals, Vance Atkinson fuel site gauges and pitch trim actuator system, Waiter’s roll trim system, Davenport’s extended nose, Stephen James “Wortmann” main gear fairing, Sam James’ construction of Gary Hertzler’s wheel pants, Todd Silver’s improved canopy design, the Cozy Girl’s torque tube offsets, Feather Light and Aerocad’s improved strake kits, to name a few,  And that doesn’t even take into account the RAF approved mods, all requiring another set of plans: Ronzc canard and HIgh speed rudders with hidden bullhorns.

My point in all this is that the Long-EZ is unique in that they’re an amazing number of variables that must be dealt within each build, and each variable requires time in research & decision-making to figure out.  I haven’t built an RV, or a Kitfox, or any other kit plane, but conventional wisdom dictates that following the instructions of “Bolt A to B, C to D, and step 15 is complete” is an entirely different construct than what Long-EZ builders contend with.  After reviewing my fellow builders’ websites, I can tell you that each plane is so amazingly unique, that they are all truly one-of-a-kind works of art!

I digress.

This all affected me today in a real way.  As I was trying to “simply” figure out what electrical components would reside in the nose battery compartment, and the configuration, placement, fitting of such components, I was of course referring back to my electrical diagrams.  I pulled out my lighting systems diagram.  It was old, outdated and not representative of the components I have on hand.  I updated it with my chicken scratchings.  Then I referred to my primary electrical system diagram, adding a ton more chicken scratchings and notes to the pre-existing myriad of handwritten notes.  And when I say myriad, I really mean A LOT!

If you’ll note the trend, I had had enough.  I was fed up with working off of old wiring diagrams.  How old?  My primary electrical system diagram was dated Jan 2014… almost 2 years old!  I had to remedy this.  I fired up my CAD program and spent a good 3-4 hours updating four electrical diagrams in my wire book.

In my mind, I think many could claim that clearly the wiring diagram is not an overly tangible thing right now in the build considering I haven’t even finished construction on many major parts of the aircraft.  What updating those diagrams did was give me better clarity for figuring out what was going where, and why.  Again, IMO, with so little space available for the amount of stuff I’m cramming into this bird, combined with the issues that plastic birds are prone to have with those nasty little electrons, not to mention RF monsters just waiting to get nasty in our headsets, I’m really trying to optimize my electrical system as best possible.

The last thought I had on this was when I had finally decided to mount the battery buss on the aft side of Napster vs. in the battery compartment.  After I checked the fit and mocked up the buss and the relay to see where they should go, I spent at least a half an hour figuring out the hardware to use to mount the damn things!  To me, this is the stuff Tony is talking about.  A half hour sorting through screws and bolts and washers just to figure out WHAT I NEED TO ORDER!   . . . amazing!  Again, this is not stuff that comes in that giant crate sitting in your driveway, pre-configured, pre-designed and just waiting for you to mount item A to pre-drilled panel B, with screw C, washers D & E, with nut F.

But I wouldn’t trade it for the world.  Good times!

Oh, btw, in case you were wondering what’s going on with the actual nose build,  I measured out my foam panel requirements for the battery compartment floors & sidewall pieces.  I should be starting on those within the next day or so.

(I also spent a good hour consolidating and organizing my electrical parts containers… also something LONG overdue!)

And hey, thanks for “listening” . . . sometimes ya just gotta ramble!

Rock on Brothers!

 

 

Chapter 13 & 22 – It’s electric Baby!

Again!

Here’s another shot of the installed & wired NG30 Aft Nose cover … not sure why I took this pic, or if it’s a holdover from yesterday, but here it is for your viewing pleasure!

Mounted NG30 cover & gear wires

I also thought I would throw this up on the site before I threw it away.  It’s my original chicken scratching diagram of the EZ Nose Lift nose gear wiring.

Initial chicken scratchings

Finally, as for diagrams, I spent a few hours last night and a couple hours this morning making sure that I had my connector pins diagrammed out on paper.  As of right now, I have about 7 AMP CPC connectors planned for use in my electrical system: the Infinity stick grips, throttle handle switches, etc.  Each of those will have a pinout page depicting information on what wires are where & wire colors, and what connectors are being used, pins, sockets, notes and any pertinent info.  Below is the first iteration of the P2 connector. Also, in addition to the P2 connector diagram, I finished the P1 diagram.

P2 Connector Pinout Diagram

Later, while watching some football today, I took my list of wire label codes that I spent a couple hours last night researching & building to use to print out a bunch of wire labels.  I’m fairly certain that I’ve already spelled out my code schema in detail here on this site, but after I work any wrinkles and kinks out of the system, I’ll touch base on my wiring code again.

In essence, I have two 6-digit codes separated by a dash that make up a wire label and then heat shrunk to the wire in an oriented sequence to depict where the wire is coming from & going to component-wise, and what location in the aircraft the wire is coming from and going to.

Printed wire labels

Here are the wire labels cut and ready to heat shrink onto the wires.  I have them in pairs because my standard is to place a label about 6-8″ from each end of each wire.  On longer wires there may be a third label thrown on approximately halfway the length of the wire.

Cut wire labels

My first test case for the heat shrink wire labels was the landing brake wiring.  I was very impressed with the legibility of the labels and the ease & speed of the whole process from printing the labels to heat shrinking them into place.

Landing brake wire labels

Since I have the nose gear wiring harness mocked up, I didn’t heat shrink some of the wires in place.  I merely shrunk them down to a significant degree, maybe 80-90%… enough that they wouldn’t easily slide off, but that I could still slide them in their final locations (past the Adel clamps) later and then do a final heat shrink to keep them in place.

Below left is the pair of AEX power wires with incompletely shrunk wire labels, while in the right pic those labels were heat shrunk down to their final position.

Wire labels shrunk 90%Wire labels shrunk in place

Here’s another couple of pics of my wire labeling endeavors this evening.  The labels in the top pic are in their final location, whereas in the bottom pic those labels will be moved into their final position and given a final pass with the heat gun later.

Wire labels shrunk in place

Wire labels shrunk 80%

I then moved on to a dirty little task:  I cleaned up the ugly layups on the aft screw posts (or tabs), and then cut some of the foam away near the remaining good glass to create a trough for flox to go into to create stronger flox corner.

Here’s the left side aft screw post prepped for glass.

Ugly duckling

And here the right side aft screw post prepped for glass.  Oh, and I guess I should have mentioned that I intentional set these posts very slightly inboard so that I could lay up a ply or two of glass on the front (outboard) side while still being able to seat the aft cover end around the posts.  I did this by applying another 3-4 layers of tape –to emulate the thickness of BID–on the inside of the aft cover when I originally 5-min glued these screw posts into place.

Gnarly glass!

I only used 1 ply of BID after apply flox into the trenched edges, but the glass didn’t want to stay down so I forced it into place using clothespins.

Ugly layup round #2

Here’s a shot at another angle.  I’m calling this ‘Ugly Layup Round 2.’

Ugly layup round #2

Tomorrow I’ll start on the remainder of the nose to get it completed.