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Section Hours: 73.9 Section Status: On Hold



Page 2, Step 1:  Flute, adjust & straighten all the ribs.

January 20, 2007:  Well, as usual, one of the first steps is deburring… notice the grin… remember it… it won't last long…



Here Angela is diligently deburring the leading edge ribs.  Her smile went away about 2.3 nanoseconds into it… this girl is all business!



January 21, 2007:  Aaaannnddd, there was even more deburring today… we learned from the horizontal & vertical stabilizers if the nose ribs aren't deburred fairly well on their nose, they have a tendencey to scratch the skin when clecoing them in.  So, we got them mostly deburred, and then Angela started straightening the flanges, and then...



… worked on fluting the flanges.  These nose ribs for the wings have the most pronounced warp due to the flanges we've seen so far… so fluting took a little while.




January 26, 2007:  Angela got back to work on the wing outboard leading edges.  She focused on getting the right one to the point of the left… more straightening of the flanges, and then fluting.




Here's a simple little idea we came up with to help with straightening the flanges… I say straighten, when I'm actually talking about making sure the flange of the rib is 90 degrees to the web.  So, we cut out a small piece of plywood, and then cut an internal 90 degree angle to use as a gauge.  You simply hold one of the edges flush against the web, and slide the gauge across the web until it touches the flange.  If the flange is flush with the other edge you're good to go... if not, adjust accordingly.  Here this one needs a bit of adjustment...




There, that's a bit better!




There, all the ribs are straightened, and fluted, ready for preassembly.

Page 2, Step 2:  Fabricate the J-stiffeners.

January 27, 2007: So, now that the ribs and splice strips are all in, it was time for the J-stiffeners.  These got cut down to 76 1/8" and will line the upper skin of the outboard leading edges.  Once they were cut & deburred, I marked the rivet line on them the same as we did for the tailcone stiffeners.
Page 2, Step 3:  Modify 4 of the ribs (2 per wing) to clear the main wing spar bars.

January 21, 2007:  While Angela was working on fluting the rib flanges, I stole 4 of the ribs from her to make the cutouts that will fit around the spar bars.  Here you can see one of the ribs before (on the right) and one after the cutouts were made (left).
Page 2, Step 4:  Build cradles to hold the leading edges during assembly.

January 19, 2007:  These were the first things we did in this section.  We were doing other woodwork and since the garage was littered with sawdust already, these just made sense.  We cut the VB-11 wing leading edge blocks and, while we were at it, the flap cradles as well (used later for the flaps), out of some plywood.  After that we cut a few 57 1/2" long rails out of some 2x2's we had laying around and then used them to assemble the cradles... and there you go, thats it... they'e together and ready for the leading edges... bring'em on!
Page 2, Step 5:  Separate the splice strips from the fuel tank skins.

January 26, 2007:  The inboard-most rib on the wing leading edges gets a "splice strip" sandwiched between it and the skin.  This splice strip serves as the outboard mount for the fuel tanks.  It will have a bunch of nutplates on it that will receive screws from the fuel tanks.  The fuel tank skins (pictured below) are a bit thicker material, and the splice strips are made from this thicker material.  So, we needed to separate the splice strip from the fuel tank skins.



Page 2, Step 6:  Deburrrrrrr...

February 12, 2007:  In preparation for deburring the stiffener holes I noticed there were a lot of scratches on them from the manufacturing process.  These look pretty ugly and it’s the first stiffeners we've seen that had them this bad (these are the same type stiffeners used in the tailcone)… The scotch-brite wheel handled them pretty well.






February 11, 2007:  I deburred the ribs and dimpled the holes in them on the same day.  In order to speed up the process of removing scratches from the ribs, especially those scratches up in the bend between the web and flange, I borrowed one of the hints I read on the VansAirforce forums.  This is just a little 1" scotch-brite wheel in our drill press.  This works very nicely and allows you to keep 2 hands on your work... much more control.




February 16, 2007:  The skins were the last things deburred.  I took a file to the edges to knock the burrs off, and then followed that up with a scotch-brite pad.  I then completed step 8 on page 3.
Page 3, Step 1:  Remove the vinyl from the inside of the skin.

February 13, 2007: This took longer than it should've… the wing kit has been sitting for almost a year, and the vinyl seemed like it didn't want to come off.  I got to do this solo this time, and with the curved skins it was a nuisance… REAL productive work here!  Anyway, we actually did this after everything had been clecoed together, final drilled, and torn back down.

Page 3, Step 2:  Cleco the ribs & splice strips to the skins.

January 21, 2007:  Here you can see we've got most of the ribs clecoed in the left outboard leading edge.  It's missing the most inboard rib (farthest away in the picture) because we still need to separate the splice strip, that gets sandwiched in between the rib and the skin, from the fuel tank skin.  We'll get the right side leading edge to this point at a later date.




January 26, 2007:  Here Angela is attempting to cleco the inboard most rib and the splice strip to the left outboard leading edge skin.  These proved to be quite difficult to get eveything lined up.  She eventually resorted to trying the right side to see if it was just as difficult... it was.  We looked them over to see what the issues were, and it appears that you need to be a bit more precise with your fluting, deburring, and flange bends on these.  Sounds like a good thing to work on tomorrow ;-)




January 27, 2007:  First up today was to get the inboard-most rib installed in each of the outboard leading edge assemblies.  As mentioned yesterday, these proved to be a pain.  I pulled them out, adjusted the flutes to get all the holes to line up perfectly, spent a bit more time deburring the nose flanges, and then readjusted the flanges to make sure they were 90 degrees to the web.  The fit in the skin was better, but I still couldn't get them clecoed in... the most forward part of the nose skin and splice strip pinched down a bit, and it was very difficult to get the rib far enough forward to get the holes to line up.  Then I remembered reading on the Matronics list about leaving the skin out of the cradles and only clecoing the forward-most holes on each rib.  So, I pulled the skins out, unclecoed everything down to clecoes in the front, and you know what... it works!
Page 3, Step 3:  Final drill the J-stiffeners to the skins.

January 27, 2007:  Next I slid the J-stiffeners into the slots cut out for them in the ribs.  Once in position I simply made sure the end was flush with the last rib, made sure the rivet line was visible in the pre-punched holes in the skin, and then drilled every 4th hole, clecoing as I went.  I've found on these stiffeners that drilling every 4th hole is just about right.  After I get those holes done I come back and drill the center hole in each of the gaps, and cleco those.  Then I come back and drill all the remaining holes.

Page 3, Step 4:  Final drill remaining #40 holes.
Page 3, Step 5:  Final drill screw holes in splice strip.


January 27, 2007:  While I was finishing up the J-stiffeners Angela came out to get some hands-on.  So, she took on final drilling all the rib, nutplate & spar holes in the right leading edge, while I did the left… the RACE was on!  She got a head start on me, but I eventually caught up ;-)




And the last thing we did for the night was enlarge the fuel tank screw holes on the splice strips to their final size and we also final drilled the two stall warning slot guide holes on each skin.  Vans provides two holes in the leading edge that serve as locators for where to cut the slot that the stall warning vane sticks through.  We don't plan on using the stall warning system provided in the kit since we plan on installing an Angle of Attack system instead... a wealth of info and far superior to a stall warning system!  So, the holes will simply be filled with rivets instead.
Pre-Install of AFS Angle of Attack Wing Ports
Pre-Install of Duckworks HID Landing Lights
Page 3, Step 6:  Disassemble.
Page 3, Step 7:  Countersink the nutplate rivet holes in the splice strip.

February 10, 2006:  We countersunk the nutplate attachment holes just prior to dimpling the large screw holes (see step 9 below)
Page 3, Step 8:  Debur the holes.

February 3, 2007:  Angela wanted something to do so she began the teardown and debur process.  Since I was still working on the outboard sections of the wings she basically began by pulling off inboard ribs and deburring.  Here she's showing us her freshly deburred splice strip!




February 11, 2007:  Today I worked on getting the remaining ribs in the leading edges deburred and dimpled.  Our leading edge ribs had more scrapes and scratches as delivered from the factory than any other piece in the kit so far.  This was a pain, and took a while to get out.


February 16, 2007:  On this day I first deburred the edges of the skins, and next I used the burraway tool to debur all the holes… Lots a holes!  I wanted to dimple the skins tonight as well, but wasn't able to get to it.

Page 3, Step 9:  Dimple.

February 3, 2007:  Angela is showing us how she man-handles the DRDT-2 while dimpling rib flanges… take that!




February 10, 2006:  The splice strips have have the largest holes that we've dimpled so far.  The large holes are for the #8 screws that will attach the fuel tanks to the outboard leading edges.  The plans stress ensuring these holes are 'carefully' deburred, or else cracking can be an issue.  Anyway, I made sure all the holes in the splice strips were deburred, and then countersunk the nutplate attachment holes (see step 7 above), and then finally dimpled the #8 holes.  We had 3 of them show signs of small cracks, so I used one of our small needle files to file them out.  No biggie, but I feel better about it.




February 12, 2007:  After deburring the stiffeners, and all the scratches removed I deburred the holes, wiped them down with some MEK, and then dimpled the holes.  The stiffeners are done.




February 27, 2007:  Angela and I finished up the dimpling tonight.  This is much more efficient as a 2 person job… even so, it took us a little over an hour to do both skins.  After that I drilled the AoA port holes in the left skin...

Page 3, Step 10:  Prime.

February 23, 2007:  We're experiencing very windy weather right now so this morning I prepped all the small parts for alodining so they'll be ready once the winds let up.  After that I gave all the ribs one more once over because I knew we left quite a few spots during the initial deburring.  After that I set this all aside and went to work on the fuel tanks.




February 25, 2007:  After the winds this morning let up I was finally able to get outside and alodine the leading edge parts.  Didn't have time to prime them yet, so that'll come later.  You can see from this pic the new chemicals work MUCH better than the old.  We're using the alodine full strength, and this is the result of only 15 seconds!  Sure beats 10 minutes.




March 4, 2007:  After returning home from the SportAir workshop I tried to take advantage of the last little bit of daylight by priming the leading edge parts.  I wasn't able to get all of them before running out of primer so I'll see if I can finish them up after work tomorrow.

Page 3, Step 11:  Rivet the nutplates on the splice strips.

March 6, 2007:  Continuing on with a little bit of riveting tonight, I set my eye on nutplates ;-)  Here the #8 nutplates are riveted to the splice strips.  These will be used to attach the outboard end of the fuel tanks to the outboard leading edges.



Page 3, Step 12:  Fill the stall warning slot guide holes with rivets.

March 6, 2007:  Next I plugged the stall warning guide holes in the skins with AD3-3 flush rivets.

Page 3, Step 13:  Reassemble in preparation for riveting.

March 6, 2007:  In preparation for riveting we placed the skins back in the cradles and re-assembled everything.  We'll start on the riveting tomorrow.

Page 3, Step 14:  Rivet it all together!

March 7, 2007:  Angela and I got started riveting the leading edge skins tonight.  We got about 3/4 of one of them done… taking our time, makin' em look good ;-)






March 8, 2007:  Angela & I riveted the second leading edge to about the same point as the first (instead of finishing the first).  Angela had to go so we'll finish them up next time.


March 11, 2007:  Ok, Angela & I finally finished the riveting of the outboard leading edges.  They look nice!  But they're not quite done yet.  Next up, we'll be installing the landing lights and the Angle of Attack ports.

Page 4, Step 1:  Enlarge the tie-down holes.

February 13, 2007:  On the underside of each leading edge skin there is a hole that must be enlarged for a tie-down ring.  You simply open up the hole gradually with a step drill.  I've found I get better results if I step the hole up to about 1/4" first with drill bits before using the step drill.  Since I'm doing both leading edges at the same time, I could drill both holes, change bits, drill both holes again, etc, etc...

Page 4, Step 2:  Cleco assembly to the main wing spar & final drill attachment holes.
Page 4, Step 3:  Rivet the outboard leading edge rib to the main wing spar & outboard wing rib.
Page 4, Step 4:  Rivet the leading edge ribs to the main wing spar.
Page 4, Step 5:  Rivet the leading edge skins to the main wing spar.


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