Slop was a poor choice of words, maybe flex describes it better? Here's my
thinking, let's say (just throwing out an even number not to be reflected
in actual weight) plane weighs 1000# on takeoff, each wing is tasked with
500# lift (yes I'm aware the canopy ads some), lift is created on the
downward surface of the wing, let's say a residual amount is transferred to
the upper surface of the flaperons 5#? Now factor in 10 microns of a gap in
every hinge, ball-n-socket joint, poly bushing compression, and torsional
flex of tubing. Ounces make pounds just like microns make millimeters so
estimating both to be 3mm in the raised position at the outward trailing
edge. Will that be an insignificant change of .05 mph or 5mph difference in
stall speed? It seems small but over the whole surface of them it may add
up. All my numbers should be considered X and "residual" as being greater
than 0.00X%
I hope this is perceived as an honest question, I'm certainly not
nit-picking, I'm kinda continuing the discussion last week regarding the
seemingly minor changes made over time that really bumped up the cruise
speeds.
When I go to remount the wings this year I'm considering throwing pulleys
on the roof, 5# weight and rigging it to pull up on them and balancing them
straightedge even with the underside.
I appreciate the feedback, thanks, Max

On Thu, Apr 18, 2019, 6:09 PM Flesner via KRnet <krnet@list.krnet.org>
wrote:

> On 4/18/2019 8:33 AM, Max Power via KRnet wrote:
> > or should I
> > set them down just a hair to compensate for the "slop" in the linkage?
>
> ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
>
> You don't want "slop" in your aileron linkage.  Set the ailerons to
> "match" the cutout in the wing and remove as much "slop" as possible.
> Slop could result in flutter.  Don't overthink the issue.  The airplane
> will fly regardless of built in errors. It will just fly better when
> done correctly.  With small errors you'll never know the difference.
>
> Larry Flesner
>
>
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