The aileron bellcrank has to attach with an an3 bolt to the control cable via a fitting. The pre-war Taylorcraft here, which I am using as a reference, used a thimble at this fitting. The thimble is slid into the gap provided in the bellcrank ears and simply rotates around the an3 bolt holding it in place. I am skeptical of this installation, as the thimble really isn't appropriate and causess wear to the bellcrank ears. So, I must ask the experts here for the correct installation.
It seems to me that the control cable would have had a bushing end woven or nico-pressed to the cable and inserted into the bellcrank ears. That would provide the correct bearing surface, but I believe the bushing fittings are pretty thick, requiring the ears to be spread out for a correct fit. That leads me to suspect something else was done.
Is it possible that the same rectangular steel spacers that were used in the elevator linkage ends were also required at the bellcrank ears? That would seem to make the most sense.
I checked for a thread here, but can't seem to find anything.
Expert opinions and assistance most welcomed! Your knowledge certainly helps reduce the head scratching time that takes away from the git-er-done time! Bob Coolbaugh
It seems to me that the control cable would have had a bushing end woven or nico-pressed to the cable and inserted into the bellcrank ears. That would provide the correct bearing surface, but I believe the bushing fittings are pretty thick, requiring the ears to be spread out for a correct fit. That leads me to suspect something else was done.
Is it possible that the same rectangular steel spacers that were used in the elevator linkage ends were also required at the bellcrank ears? That would seem to make the most sense.
I checked for a thread here, but can't seem to find anything.
Expert opinions and assistance most welcomed! Your knowledge certainly helps reduce the head scratching time that takes away from the git-er-done time! Bob Coolbaugh
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