by taildragger » Tue Feb 01, 2022 7:26 am
The front spar cap did, repeat DID COME WITH PRE-DRILLED PILOT HOLES in the tail kit. The quick build fuselage kit arrives April 22, 2022 so I have 11 weeks to figure it out, or should I call Sonex?
I have learned that Sonex cuts it too close on edge hole location tolerances because:
1) Pilot holes are too close to edge. E.g. Due to the "two radius rule", I had to remake the -11 root rib because it's holes were too close to the edge.
2) Sonex assumes builder understands how to build an airplane without step-by-step instructions.
3) Sonex assumes builder will hold tight tolerances on parts to be mated later without understanding the term "tolerance build-up", or "worst-case" analysis.
4) Use of hand tools while cutting and bending ribs and spars almost guarantees poor tolerance control. I have improved my understanding over time but I hope my parts all fit the "two radius rule".
5) I use a digital caliper accurate to one thousandth, but after cutting and bending a piece, still come out 1/16 off-tolerance due to pen width error and my inability to control bend radius or twist.
Two questions:
1) Can additional rivets be used when building a Sonex? This is an exception case where a rivet is too close to the edge and reinforcement is necessary.
2) Can shims be used to adjust minor and major load-bearing parts? Should they be made of steel or aluminum?
Building electric Xenos
President, EAA Chapter 1250