<<Prev Section 6 - Vertical Stabilizer Next>>
Section Hours: 40.1 Section Status: Complete



March 11, 2006:  FINALLY!  The tables are done, the lights are up, the electrical is done, the compressor is mounted, the shelves are up, the storage racks are up, the garage door is insulated, etc, etc.  Finally we can get started... only a couple months late!  There is one small benefit to being late:  Van's came out with a Service Bulletin for the RV-10 Vertical Stabilizer top hinge bracket in February.  It affects what is done on page 1 of the plans, so if we had started when we wanted to we would have been drilling out rivets in order to put the doubler plate called for in the Service Bulletin in.  Instead, we can account for it during the build... a small benefit to being behind.  Ok, so here we go... these are the parts we'll be dealing with first (I forgot to include the doubler plate called for in the Service Bulletin).  Doesn't look like much but I see a lot of holes, so I'm expecting a lot more time consuming activity than the limited number of parts would suggest.




Step 1 calls for measuring & cutting the VS-1014 Rear Spar Caps.  Sort of unnerving that the first step in your expensive kit is to cut it!  Then reality sets in... if I screw this up, this angle can't be that expensive... just do it!  Besides, we're going to need to get used to this!  After the cuts, its over to the bench sander to knock off the sharp edges, and then to the Scotch-Brite wheel to smooth it up.

March 13, 2006:  Well, family was in town so getting out in the shop was a "whenever we could" thing over the weekend.  We enjoyed the family time!  Now, back to work!  Step 2 had us clamping the newly created VS-1014-L & R Rear Spar Caps into the corners of the VS-1003 Rear Spar, and then match drilling all the Rear Spar web holes into the Caps.  Note to self: I can already tell that attention to wording in the plans is going to require some diligence.  The Rear Spar has holes drilled in both the web, and the flanges.  The plans indicate to only do the web holes now.  The flange holes come later.  Once the web holes were done, we got to try out our new hole deburring tool... not too bad.

March 14, 2006:  After clecoing the Spar Caps back in place, we now got to match drill the flange holes of the Rear Spar.  Then back off they came and back to deburring we went.  And once again, they got cleco'd back on.  Wow, no wonder I've heard when you build an RV you basically assemble & disassemble the thing 3-4 times.  I'm already believing it!

March 17, 2006:  Step 4 first calls for deburring the VS-1008 Rear Spar Doubler.  This piece has some pretty jagged edges on it so its off to the bench sander again.  A dremel tool with a small sanding wheel seemed to handle the interior cutouts ok.  The Scotch-Brite wheel handled the finishing touches on the outside edges very nicely, but the inside edges were done by hand... probably have to find another method for that...




The deburred VS-1008 Rear Spar Doubler



After deburring the Rear Spar Doubler, we got to cleco again.  This time it was the whole Rear Spar assembly including the Hinge Doubler called out in Van's Service Bulletin SB 06-2-3 (VS-1003, VS-1008, VS-1014-L & R, VS-1010, VS-1011, VS-1012, and VS-1017)


We then used a #30 drill and final-drilled all the 1/8" holes in the VS-1008 Rear Spar Doubler, the Rear Spar Caps, and also the holes in the Rudder Hinge Brackets and the new holes in the VS-1017 Hinge Doubler.  Step 5 had us using a 3/16" drill to match-drill the upper attach bolt holes into the Rear Spar Caps.




Ahhh, a new toy to play with... Step 6 has us countersinking all of the #30 holes below the upper attach bolt holes.  Since the microstop is new, it took some time getting it setup for just the right depth.  Once done, the countersinking went pretty quick.  Alright!  done with page 1... Progress!!

March 19, 2006:  Yesterday morning we went to downtown Fort Worth and witnessed the second tallest building implosion in the world.  Very impressive stuff!  After that we came home and I had a nagging headache for the rest of the day.  Annoying because I should've been able to devote a good portion of time to building.  Instead... nothing!  Oh well, we saw some good progress today.  Here's the parts list for the next couple of steps.  Looks like we're going to be putting together the skeleton of the vertical stabilizer.




And here it is, clamped to the table and ready for final drilling of the common holes.

After final drilling it was time to attach the skin in order to final drill it.  As we had heard, clecoing the skin to the VS-1013 Nose Rib was an absolute PAIN!  Even though we deburred the Nose Rib it still left some significant scratches on the interior of the skin while trying to muscle it into place.  It worries me to think how it'll be after we get a coat of primer on both of those pieces.  Doesn't sound like fun!




Here's a shot of the telltale bump in the skin I've heard so much about.  I think we're definitely going to have to sand that nose rib down a bit!




Here we can see Angela just having a blast with Clecos!




We've also heard that this is one of the first real feelings of satisfaction when building an RV... having the first resemblance of an airplane part.  We'd have to agree!

March 22, 2006:  Well, I have to confess... last Sunday when we were working on the plane we were in a hurry.  I knew there was a problem with the nose ribs in the vertical stabilizer but in our (my) haste I decided to go ahead and hang the skin.  I regret that now because there are a few permanent bumps in the skin from the nose ribs... oh well, live and learn.  First step today was to pull the skin back off of the skeleton in order to "massage" the nose ribs a bit.  I pulled up Tim Olson's "Gotcha" page this morning to remind myself of what it had to say about dealing with the nose rib issue (should have done that in the FIRST place!)  I also wrote Van's... I got 2 different answers, both which would work.  I chose to go the route of radiusing the corners as you can see here.  I wound up taking about 3/16 off of the front of each flange.




Here's a shot of the inside of the vertical stabilizer skin where the bump was.  I draped the skin over the edge of my table and lighlty tapped the bump a few times to flatten it out some.  The results were not perfect, but definitely acceptable.  I then used a Scotch-Brite pad to sand out the scratches left by the rib.  All that's remaining are superficial scratches that will come out when I give the skin a final scuffing prior to priming.




Section 6-3, Step 4 calls for final drilling most of the holes in the skin... that's a lot of holes!  (I bet the wings are gonna be fun!!)  Once I get all the holes drilled out, I think that'll be it for the night.

March 23, 2006:  I've been looking forward to getting home to work on this all day!  Ok, first step, mark the Empennage fairing screw holes... done!  Next step, disassemble the skin & skeleton... done!  Then I busted out the soldering iron and cut the "requisite" RV rivet stripes in the blue nylon film protecting the exterior of the skin.  After that I get to do the fun stuff... debur... and debur...




and debur... and debur... wait a minute... what was it I was looking forward to again???  Ahh yes... the sooner I get done with this, the sooner I'll be priming and riveting this weekend!!

March 25, 2006:  This morning saw Angela & I enjoying a cup of coffee, eating our breakfast & reviewing Vertical Stabilizer & Rudder plans.  Once we realized what we were doing we laughed at ourselves.  Next time we'll be sure and get a picture.  During the afternoon we had a few "chores" to do around the house so building didn't start until later tonight.  Angela went back to working on the website while I started off with step 8 of section 6-3.




Here you can see the the countersunk holes in the VS-1003 Rear Spar.  The marked hole is where the lower row of rivets will go that attach the Vertical Stabilizer skin.  Everything below that will be covered up by the fuselage tail skins.




Remembering that Angela was working on the rudder I thought I would go ahead and separate the R-1007 Rudder Stop parts as called out in 6-4 step 3.  She'll need the R-1007A's, and I'll need the R-1007B's (shown here).  This shot, as you can probably tell, is a before and after look.  The stamping process produces some fairly sharp edges.  A quick trip to the scotchbrite wheel and the edges are just as soft as they could be.


March 26, 2006:  Today Angela is at work again and I debated on whether I wanted to inventory the second Wing crate, test my alodining & priming strategy, or work on building... I chose the latter!  I've still got some time on the Wing kit inventroy, and I know once I alodine & prime a test piece I'm going to want to follow it up with some real parts.  So, I decided to get all the vertical stabilizer parts to a point they're ready to be primed.  There are only a few things left.  Here I'm final-drilling the VS-1015 Front Spar Doubler to the VS-1002 Front Spar (6-4 step 1).  Once done, I pulled it off and deburred the holes in each part.




Here is the doubler as I'm countersinking the 4 bottom holes to accept the dimples I'll eventually be putting in the corresponding holes in the front spar (6-4 step 2)




And here I am doing the most time consuming process of the whole day... deburring!  I basically went over every single piece of the vertical stabilizer and made sure they were completely deburred.  I was amazed at how much I had missed up until this point.  I tried a couple of different techniques, mainly to see which worked best, but also to break up the monotony of the task (I can here some of the guys out there snickering and mumbling under their breaths 'just wait till the wings').  Well, I finished the day right as Angela arived home... perfect timing!  Oh yeah, I just remembered one more thing... I still have one more thing to do before priming... we plan to eventually mount a camera atop the vertical stabilizer.  In order to do that we're putting in some conduit that will reach up to the fiberglass tip.  We'll need to cut a hole for the conduit in the VS-1006 Top Rib (the conduit will be routed through existing holes in the VS-1005 & VS-1013 Nose Ribs).  So, looks like that'll be what I'm doing next time.  THEN I'll get started on the priming!


March 30, 2006:  As mentioned earlier we plan to eventually mount a camera in the tip of the Vertical Stabilizer.  This is an idea fellow RV-10 builder Michael Sausen showed me, and I really liked it.  In order to get cables to the camera we needed to drill a hole in the VS-1006 Top Rib.  There are lightening holes in the other two ribs, but not in this one.  I consulted Van's regarding the modification and they indicated it shouldn't cause any problems.  So, using the recommended hole size (3/4") for the 5/8" conduit Van's offers I used a unibit to drill the hole.




Here is the finished product, along with the conduit installed for a test fit.  Originally I planned the hole a bit further back, but then noticed it was directly between the cutouts in the flanges.  These ribs are already pretty flimsy between these cutouts so I felt moving the hole forward between the flanges would provide a little more support.

April 1, 2006:  Originally we planned on dimpling after priming, but I think we've decided otherwise.  For now we'll dimple then prime and see how it goes.  Here 6-3 step 7 has us dimpling the flange holes in the ribs.  Here I'm using the pop-rivet dimpler to get the nose flange holes that I'm not able to get with the DRDT-2.




My original plan was to scuff all parts prior to any finishing, although now involved with the process I was kind of curious if scuffing the aluminum prior to Alumiprep would make much of a difference.  So, I scuffed some, but not the others.  This was my first attempt at the whole Alumiprep/Alodine process... not too bad I think... a little boring though.

April 5, 2006:  Tonight I remembered I still needed to dimple quite a few holes in the vertical stabilizer.  Since I hadn't done anything with the vert stab in a while I was feeling the need to get something done on it.  I breezed through the remaining ribs and spars pretty quick.  The next step was to dimple the skin (6-3 step 6).  But, since we plan to prime every inch of the inside of this plane, I wanted to scuff the surface first...




Next came the dimpling of the skin.  This was my first experience with the DRDT-2 on a skin... actually, my first experience dimpling a skin, period!  I liked the idea I had seen on some other sites about laying the skins on some foam to protect it while dimpling so I set up my tables to accomodate this (sorry, I was in a hurry tonight so no pictures).  The foam did a wonderful job, as I expected, of protecting the skin from scratches.  However, one thing that surprised me was that the foam caught the edges of the blue nylon film where I had cut the strips out for the rivets (I was dimpling with the male die on the bottom so this put the nylon on the foam... don't ask... I was experimenting...)  Anyway, I didn't realize it at the time, but here are the results... ... nothing major, just thought I'd mention it for consideration.  Another learning experience...  Well, we're off to Sun-N-Fun this weekend, so no building.  It's our first trip there so we're pretty excited!!  I'm especially excited about checking out the glass-panel vendors, as one of them will definitely be going in our bird!!  Plus, we're going to try like crazy to get a demo ride in the factory RV-10.  We'll post some pics when we get back too!

April 15, 2006 (6-4 step 5):  So, we decide last night we'd get up early and get all the parts Alodined before heading off to the local EAA Chapter meeting.  I don't have a picture of it here, but one thing that concerned me is we used a screen door to hold the parts as we rinsed them off last night.  The intent was for them to be on the screen just long enough to rinse them, as they would be Alodined soon after.  Welp... we wound up storing them overnight on the screen door (DOH!)  Some of them had some pretty interesting designs in them this morning.  We wiped them down and proceeded with the Alodining just to see how they'd turn out (the spots visible on the spar below are where I sanded out some scratches prior to Alodining)




Ok, back from the chapter meeting... some good info on fiberglass work, and met a lot of new people (only our second time there).  I also took one of our parts affected by the screen door fiasco with us and showed it to our tech advisor... he seemed to think it was fine, especially since we still plan on priming it.  That's my plan for the rest of the day, to get all this stuff primed!  First, I needed a nap... we didn't get much sleep last night... I guess I needed it more than I thought because 2+ hours later, I still wasn't ready to get up, but I reluctantly did.  Anyway... I roll out into the garage, and start getting things set up for priming... 




I haven't ever used a spray gun before, so that took a little getting used to!  I think I still need some work though... a bunch actually!!  Man... this was a frustrating week for me... it was a learning week... a lot of time spent on stuff that didn't seem to produce a lot!  And the stuff we did do, didn't seem to come out to our expectations.  I primed tonight for the very first time... it left a lot to be desired.  I planned to get it all done tonight, but that didn't happen.  It was windy, so I wasn't able to open the garage door for fear of stuff blowing all over the place (yes, it's that windy outside).  I usually open the door about 6 or 8 inches in these cases, and even then you can feel a breeze inside the garage.  That being the case I decided we were good to go for priming so I went at it.  After the first round I sprayed some thinner through the gun to clean it out... I don't know if anybody reading this has used the AKZO recommended TR-19 thinner before, but let me tell you that stuff is POTENT!  I didn't realize it at the time (my filter mask eveidently works exceptionally well!) but the fumes from this stuff were phenominal!  I came in the house, took off my mask, and inside of 30 seconds, Angela was remarking about the fumes... from the other side of the house!  Lesson learned... All priming will be done outside, or at the very least with the garage door completely opened!  We're letting the garage air out now, and will continue the priming later!  Another lesson learned/decision made... our original priming strategy was to Alodine & prime all non-Alclad parts, and only prime the Alclad stuff.  We completely forgot that most of the spars and ribs are made out of Alclad sheet (DOH!)    If we'd realized this, we'd have saved ourselves a lot of time this week by not having to Alodine 90% of what we did... oh well... frustrating.  Good thing is I've learned a lot this week... a lot!
April 16, 2006 (6-4 step 5):  Realizing I hadn't taken any shots of the parts after priming last night, I decided to get a couple this morning before Easter morning services.  You can see the disappointing results... The parts are completely covered, but the primer is almost translucent.  Hmmm... I'm obviously not doing something correct (?)

Ah-Ha!  I figured it out... the AKZO primer directions indicate there is a 30-minute "induction time".  I have heard this implies mixing the 2 parts and then waiting 30-minutes before using it.  Last night I did not do this.  Tonight, after returning from Easter with the family, I decided to finish up the priming.  This time I did let the mixture sit 30-minutes prior to using, and the results were immediately noticeable!  This looks more like it!

So, cool!  Now we're ready to get on with some actual assembly... things are going to be exciting next time :-)
April 17, 2006 (6-5 step 2):  Tonight Angela had a soccer game so I planned to mow the lawn, and do some other things around the house.  When I got home I found out the sprinklers had run... oh well, can't mow the lawn when the grass is wet... let's squeeze a few rivets ;-)  Dont tell Angela!!  We agreed we'd start the assembly tomorrow night.  So, I did the other things I needed to do, and then snuck out in the garage to see how the squeezer worked!  She won't mind if I just do a couple... hehehe...

(6-4 step 6):  Ok, so I was busted!  She got home right as I started.  Well, I couldn't have all the fun.  Besides, she was happy to just be able to walk up (still in cleats!) and squeeze a few rivets... no setup, no fuss!

So, will I mow tomorrow night... probably not ;-)
April 18, 2006 (6-4 step 7):  Had a little fun with some rivets tonight :-)  I thought I'd get a little more done than I did, but oh well... I had a little fun tonight!  This is the rear spar assembly for the vertical stabilizer.  It is what carries the main loads of the vertical stabilizer, and is also where the rudder attaches to the plane.




The rudder hinge brackets attached with 4 rivets each.  The two that fit closest to the bend in the bracket proved to be a little too close for the diameter of the dies we have for our squeezer.  So, what's a guy to do... bust out the rivet gun & bucking bar for the first time!  Btw: what's wrong with this picture??  The experienced ones in the bunch are probably already snickering...




Well, when you precariously suspend a part between two tables with no clamps or any other method of holding it still, unless you're lucky (as I guess I was on the other 10 rivets) this is the result!  On my second to last rivet, as soon as I pulled the trigger the gun bounced across the part (DOH!)... live and learn (again...)




Here's the completed rear spar assembly.  One thing of note: I stepped up a rivet length on the rudder hinge brackets.  The longer ones were a little long, but by the same amount the shorter ones were short (make sense?)... so posed with the option of a little short, or a little long, I chose a little long.  Also, the previous picture shows the hinge doubler called for in SB 06-2-3.




4/19 UPDATE:  After browsing a few of the other builder's sites I realized something... Other than the flush mounted rivets, there is no specific indication in the plans of which direction the rivet head should face on the rear spar assembly.  This means I should've thought about it first before just simply inserting the universal head rivets the same direction as the flush ones.  Had I done that, I would've realized that the side I have the shop head on is the exposed side (open to the rudder) and simply turning them around would've put the shop head inside the vertical stabilizer skin never to be seen.  Plus, I wouldn't of had to use the rivet gun.  Bet I remember to think about it in the future!  I guess if it was going to happen sometime, this was probably one of the best assemblies it could've happened on.
April 21, 2006 (6-5 step 3):  Over dinner I took one final look at the rudder plans to make sure we're ready to proseal the trailing edge.  Turns out the only thing left was to put the slight bend in the trailing edges of the skins... Let me tell you, that was slightly nerve racking for me... don't know why, but it was.  I think it actually went ok though.  So, now, done with the rudder... only thing left before busting out the pro seal is to assemble the vertical stabilizer skeleton.  Then we'll call it a night and pro seal tomorrow.  Kewl!

April 22, 2006:  With just a little remaining working time on the pro seal after the rudder trailing edge, I began dabbing the stuff in between some of the lightening holes on the vertical stabilizer front spar where I wanted the conduit to attach.  I also put some on the on the top & middle ribs where the conduit goes through them.  One thing I learned about pro seal (actually tank sealant is what they call it) is that they weren't joking about 30-minutes... I finished in time, but at about 30-minutes the stuff definitely couldn't be spread any longer!




Once we were done for the day, I went back out to take a couple of shots.  Here's a shot of the vertical stabilzer with the conduit set in it's final position.  In a day or so when the tape is removed this stuff won't be going anywhere!

May 7, 2006:  Can't remember if I mentioned it already or not, but the reason it took so long for me to get back to the vertical stabilizer is because of clecoes and oversized holes.  A little while back I went to cleco the skin on the vertical stabilizer and the clecos would just pop right out of the holes.  Long story short, the holes are ever-so-slightly oversized and the clecoes (as was suggested to me by numerous people on the VansAirforce forums) were of the 'cheaper' variety!  So, we ordered some "Wedge-Loc" clecoes from Cleaveland Aircraft Tools (other suppliers carry them too) and waited for those to arrive.  In the meantime I finished up the rudder.  Welp... we've since received the Wedge-Locs, and finished the rudder... so here we are... time to get back on the vertical stabilizer!!  Time to finish this puppy!!  (The Wedge-Locs work GREAT by the way!)

(6-6 step 2):  Riveting the skin on the vertical stabilizer is a puzzle.  You have to rivet the first few sections of rivets in a specific order or else you wont be able to gain access to other rivets... seriously!  So the first step was to remove the bottom nose rib.  This allowed us access to the middle nose rib.  Its interesting... the middle nose rib turned out to be the toughest part of this thing to rivet, but if you build this thing according to plans, its the very first thing you rivet!  Kind of intimidating!!  Anyway, Once the nose middle nose rib was done, I noticed I marred the thing up in a few places so I used our powder-coat touch up paint to cover the scratches I left in the primer.  The touch up paint was quicker than mixing up some of the primer.




(6-6 step 3):  After the middle nose rib came the top rib, but only the portion forward of the front spar.  Angela wanted a piece of the action too so I let her do this one.  She then threatened me with the squeezer so I let her do the bottom nose rib too ;-)




(6-6 step 5):  After all the nose ribs were in place, next came the entire front spar.  Relative to the rest of the airplane this isn't that many rivets, but it sure seemed like a lot at the time!  All of these were done with the rivet gun and bucking bar.  Here I've got the rivet gun on the outside, and my left arm is inside the vertical stabilizer where I'm holding a bucking bar on the underside of the rivet.  The rivet gun basically pounds the outside of the rivet while the bucking bar bounces off the backside of it.  These two forces basically work against each other to compress the rivet clamping everything (the skin and spar) in between the two ends.  These rivets are tiny, tiny, but strong... and there are a ton of them!




(6-6 step 6):  Once the front spar was completed on both sides, then came the middle rib behind the front spar, and then the remainder of the top rib.  The middle one had to be done with the rivet gun, but the top one could be done with the squeezer.  Until I get a little more skilled with the rivet gun the squeezer is my tool of choice!  This is a shot of the middle inspar rib from inside the vertical stabilizer.




(6-6 step 7):  Now the the middle inspar rib is complete, all the ramaining rivets can be done with the squeezer (yeehaw!)  Next step was to put the bottom rib back in place and rivet it in.  Once that was done the final skin attachment was to the rear spar.  After the skin was completely attached there were about 30 more rivets that attached the flanges of the rear spar caps to the flanges of the rear spar.  After those we could stick a fork in it... it was done!!!  Here I'm using the squeezer to set the 1/8" rivets attaching the bottom inspar rib to the rear spar.




And... drum roll please... here they are... Our completed vertical stabilizer and rudder!  Some day these babies will be controlling the yaw in our very own airplane!!  Ahhh we can dream can't we...  Is it too early to make airplane noises yet ;-)



Home Log By Plans <<Prev Next>>