Moving to the main wing panels, the inner ailerons suffered from the same malady as the tip ailerons, with the same results: Significant double-centering, excessive load on the servo, and limited upward surface movement. The OEM linkage geometry is a bit less of a problem here, as the wing is slightly thicker and thus slightly more moment arm. So, I decided to see if just addressing the wiper and sub-TE problems would cure the symptoms.
The process was identical...disconnect the linkage rod, then pivot the aileron down about 70-80 degrees, and secure it in position. Re-shape the wiper (to the extent possible) by extensively block-sanding with 180 and then 220 grit. These wipers are also molded with the wrong profile, so re-shaping ability is somewhat limited. See the pics for an idea of how grossly out-of-profile and thick they were. As I previously stated, completely unacceptable.
Next, the sub-TE overhang was reduced approximately 1mm by marking the new profile with blue tape, and using a thin sanding block to sand the edge to the new line.
With the OEM linkage back in place, there is still very slight double-centering (less than 1mm), but surface throw is correct with only minimal binding. It really does need new linkages here as well, and I will likely do that at some point in the near future. For now, it is adequate to get the plane flying. Next, we tackle the flaps (all 12 linear feet of them)...
The process was identical...disconnect the linkage rod, then pivot the aileron down about 70-80 degrees, and secure it in position. Re-shape the wiper (to the extent possible) by extensively block-sanding with 180 and then 220 grit. These wipers are also molded with the wrong profile, so re-shaping ability is somewhat limited. See the pics for an idea of how grossly out-of-profile and thick they were. As I previously stated, completely unacceptable.
Next, the sub-TE overhang was reduced approximately 1mm by marking the new profile with blue tape, and using a thin sanding block to sand the edge to the new line.
With the OEM linkage back in place, there is still very slight double-centering (less than 1mm), but surface throw is correct with only minimal binding. It really does need new linkages here as well, and I will likely do that at some point in the near future. For now, it is adequate to get the plane flying. Next, we tackle the flaps (all 12 linear feet of them)...
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