There's no need to torque the crap out of any of the wing attach fittings through the spars, or even WAF to WAF, for that matter. They are simply "pin joints" in engineering terms, meant to keep things from moving around. Friction is not even considered when analyzing the stress on these things, even in the case of the WAF to WAF connections. NASA doesn't even consider friction in stress analysis of critical structures, at least that's been my experience. If you start crushing wood, you're over tightening. Don't bother with torque charts....that is not the proper "case" for these bolts, given that they can easily crush the spruce.

Mark Langford
Mechanical Engineer....RETIRED!
[email protected]
http://www.n56ml.com
Huntsville, AL
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