Structural Testing Of Homebuilt Aircraft
At each step they do not follow exactly that ideal to activate flaps or ailerons? Think
(20, 60, 80, 90, 95, 100%), we wait a line. Nothing wrong with that either, about it. In our experience, a good
couple of minutes for the wing to as long as discrepancies are not wing should show a permanent set (2)-
"settle", before taking readings. After ridiculously large. The more careful (14) that is less than 1% of the
that we begin to gently and symmetri- we were during the testing and the maximum deflection (14)-(15).
cally unload the wing, stopping at the better tools we were using, the more With that we can disassemble the
same loads as we did on the way up, consistent these test points will testing set up and examine the fit-
and take readings again, again each appear on the diagram. tings as mentioned earlier. If nobody
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