Hi marc,
I am frustrated because I almost made the same mistake on both sides. The explanation on the drawing is misleading (not complete) for a beginner. I have started with the LH and screwed it. The only way I can imagine being able to use the reamer properly, is to have the inboard end wing ribs removed. The guiding block shall also be removed leaving only the inboard main spar in place for wing rigging. Otherwise there is no room to properly use the reamer!
The RH rigging (done second) would be OK but I can feel a little loose in the wing because the main spar bottom hole is enlarged a little (.003in). The pin penetration problem is the same as explained below on the LH.
The problem on the LH is much worst; the pin assembly is shifted because the hole locations on the 4130 plates are offset (see pictures 1301-1302-1303) therefore the lever is out of alignment. Please note that pic 1301 shows the distance (.650in) of the outboard spar bottom hole from the edge, yet the distance (pic 1302) of the main spar hole is offset creating the mismatch of the lever (pic 1303). In any case, I now have ruined the 4130 plates holes on the LH. Please note that with the spar option, the holes come pretty much near the final size not 1/4in as mentioned on the dwg (at least on the outboard spars) and that does not help since there is no room for error. My top main spar bolt holes are OK. I also noticed that when all the bolts are tightened, the wing is hard to rotate up and down. Should there be a minimum gap? I noticed that the demo plane was easy to rotate did they used some lubrification? The rear spar slot is also very tight when the bolts are tightened and prevent the wing from closing in place properly.
I spent much time thinking about all this and the only solution that comes to my mind is to replace the 2X 4130 plates. At least on the LH as the RH might be OK if I use a larger reamer and a larger diameter pin (the lever is well aligned). This is overall the hardest part of the assembly up to now.
Questions raised to Sonex; what is the cost and delivery time for these 4130 steel plates and new guiding block (LH)? What is the maximum concentric play allowed on the locking pin holes? Should the wing be tight without any play vertically (on the drawing there is no tolerance)? Should the locking pin penetrates more (barely being supported by the AFT plate)? If yes, should the guiding block be countersunk to allow more penetration?
I hope we will all learn from my mistakes...
- DSCF1301sm.jpg (119.83 KiB) Viewed 25432 times
- DSCF1302sm.jpg (116.86 KiB) Viewed 25432 times
- DSCF1303sm.jpg (122.88 KiB) Viewed 25432 times