A call to Vans

I called Van's in the morning and explained my situation. Support said that it was not a critical structural area. He said it was unfortunate but all will be ok as its just a web attachment point to a spar. Build on.

I reasoned on the matter throughout the day. I felt much better after talking to Van's Support. The area is well exposed for periodic inspections. The edge distance is just under the minimum on the flange by a hair. I also measured the HS00001 doubler and found that the hole in the doubler is still within the minimum specifications for edge distance. Although it is not the most ideal situation, still its not that bad. I really don't want to take another step back, but I will chalk it up to a lesson learned.

Below is the picture of the edge distance issue. Looking at the top most hole on the flange; the rib on the right is correct, while the rib on the left is just a bit too tight for comfort. Very very close...

If anything I can always run it by the very experienced eyes in the local EAA group.

Build on.

Just about finished assembly of the HS - 3.5 hours

I started off the evening working on the left side HS. I fitted the new HS00005 and 000006 ribs to the assembly. I checked, checked and re-checked the fit before i started to drill. My first set of holes were in the aft flange of HS00005.  Then in the aft flange of HS00006 through to HS00005. I was very pleased with how everything lined up. 

I then noticed that my edge distance on my top hole of HS0005/00006 was just a bit high about 1/16". I was a tad bit concerned about edge distance. The holes line up perfectly....although getting these holes drilled perfect is extremely difficult. its hard to get the appropriate dimensions in there with the skin on and all the surrounding clecos. At worst I have an edge distance of 0.209" (0.155" from the edge of hole to edge of rib) on the top most #30 hole in the forward flange of HS00005 where it attaches to HS-710. I see the listed edge distance minimum is 0.219, so I am just ever so slightly over the limit.  I will email vans and double check that I am ok.

(Darn...what its a tough spot to drill and there is little room for error!!)

UPDATE: See October 22, 2014.

I finished up by cleco'ing the HS assembly together. Whew....Just about done. All I need to do is drill the holes outboard of the bend line in the front spar.

I took the skins off the HS and started to double check how straight everything is. I will save the drilling for another day as it is getting late.

First EAA chapter 30 meeting

Tonight was my first EAA chapter meeting. The group was a bit larger than I thought there would be. The president of the chapter gave a presentation of his recent trip to New York filled with tons of little tips. Met a couple of nice folks. Mike is working on an F1 rocket and is just a bit farther ahead than me. Jim, was eager to help with advice. In just a 10 min conversation I picked up more from him than I have in 30 hours of building. The EAA chapter is just a great resource.

A bit more work in the left HS - 1 hour

Not a whole lot to report for today. Managed to cleco the skin on the left side of the HS, ready to complete the HS00005/00006 ribs. Unfortunately I have brought work home and that and the kids have taken president for the weekend.

HS assembly right side ongoing - 4 hours

I started off the evening working on the new HS00006 ribs. I decided to order new ribs when I decided to redo the front spar. I'm sure the old ones were fine, however I wanted to be sure that each piece had a correct fit. and for $20...why not start fresh.

 I marked each one left and right and then trimmed each according to the plans. I drew centre lines and then drilled my holes.

I then moved over to the HS angles. I was very careful this time to not take too much material off. I ran them threw the band saw. I was nervous as the band saw is a little ravenous at times if you are not paying attention. But I went slow and in the end...I didn't mess up.

Then I bent the angles to 6 degrees each end.

I cleco'd the right HS assembly together and then put the skin on. I worked the HS00005/00006 ribs. I drew all my centre lines out and ensured that all lined up. I then started drilling holes as per the plans.

After I was done drilling, I was very happy to see how the holes lined up in the front flange of HS00005. The top and bottom holes are a bit blind and its tough to get them to line up. I checked, checked, and re-checked before I drilled. And the proof that it worked shows.

Tomorrow I will finish off match drilling the new parts. and hopefully I can complete the left side....again.

Building tip - In retrospect, the evening took quite a bit of time. But I proved to myself that the front spar of the horizontal stabilizer is something that you just don't rush if you want to have straight even holes. The key to everything so far on this portion of the project is to slow down.... (The VS and the HS rear spar gives you a bit of a sense that you can rip through pretty quickly). For  this...slow and straight!!!!

Mark centerlines on almost every part. Draw centerlines on the table and then as you cleco...it becomes clear how straight you are. Then when you start clecoing parts together. lines are visible through holes and every little bit helps ensure straight! Use a drill press! Hand drilling through thick materials ends up with slightly crooked holes. And lastly....read the instructions, and the plans, and then read them again....and only then...start working.

Working away on the HS front spar... Third times a charm - 1.5 hours

Not a whole lot of time available to work on the plane tonight. So I jumped back to the horizontal stabilizer. I received the replacement HS-710 and HS-714 angles from Van's yesterday. (Grrrr..The third ones!!!) I hope I really nail it this time.

I carefully marked out the center lines on each side of the angle pieces. Then I countersunk the two center holes of each angle (Very much a pain to re-set the countersink cage after I changed it for the rudder counterweight)  I then cleco'd the front spar assembly back together and ensured that the assembly was straight. Everything was bang-on! It really helped when I filed the ends of the front spars where they met on the previous Friday. Now with the new angles...it all lined up. 

I used the drill press and matched drilled all the holes inboard of the bend lines with a #30 bit. Once complete I then rechecked the front spar assembly and confirmed that it was perfectly straight even when sitting vertically on the HS-714 angle. I can safely say that I did less than 1/32" difference between the two ends. I was pleased with the fit of the countersunk holes as well cause its really tough to get it to nest nice.

Third time's a charm!! Like my tool box... Ahh...I just have to laugh! Well...At least it's perfect.

Do I have a name for the plane now??? We shall see.

Prepping the rudder skins, stiffeners and the Verticle Stablizer - 2 hours

I can't progress much further on the rudder unless I rivet the stiffeners to the rudder skins. I laid out the stiffeners on the rudder skins to ensure that the stiffeners did not interfere with the rudder spar and trailing edge.

I then worked on the fit of the rudder skins around the R-405PD rudder horn. The skins were a touch too tight, so using a small flat file I carefully enlarged the opening. I was pleased with the fit of all pieces.

I then began to scuff up all the rudder stiffeners, rudder skins as well as the Vertical Stabilizer pieces with red scotchbrite pads.  

I noticed that the VS-707 had a point of impact with something located almost directly in the middle of the part. Something sharp had struck it. I'm not too alarmed, but I figure that if I drilled out the point of impact with a small #40 hole, this would relieve the stress point and shouldn't cause any issues. My thinking is that this would be no different than a tooling hole like on every other rib.

UPDATE! - (October 15th) I have received a confirmation e-mail from Ken at Van's that my proposed solution will work just fine.