Long time listener first time caller.. Recently, I purchased a really nice 1946 85 hp BC12 that's been fun to fly and interesting to maintain. (particularly that time one of the tail wheel springs came off on landing, but that's another story lol)
My airplane had an extensive rebuild before my purchase and is generally in great shape but it came to me with an inop trim tab indicator. One rainy day I decided to take it upon myself to investigate why the trim indicator wasn't working and cranked the trip to it's stop not knowing this would jam the trim tab if the elevator wasn't in the neutral position. After reading several helpful post here by Robert Lees and many others I discovered my folly.
Due to the kind folks writing about their experiences I discovered that by loosening the tension on the trim cable that one could reset the trim tab to neutral by turning the pulley/jackscrew shaft at the rear.
I'm wondering if anyone could help a simpleton understand what is happening in that jack screw when this jam happens? I'm assuming the screw has reached its end? in this case its bottomed out and I'm assuming that if one where to have turned the trim wheel in the opposite direction the jack screw would have come out of the threaded portion of its carrier? Is that correct?
Lastly, why does this only happen when the horizontal stabilizer is out of the neutral position?? I understand that the travel is limited by the spring tensioner at the rear and the limiting bolt at the front of the trim wire but it makes me a little concerned for making large adjustments while in flight, like for slow flight/stall training.
Many thanks for your thoughts, this board is a great resource.
My airplane had an extensive rebuild before my purchase and is generally in great shape but it came to me with an inop trim tab indicator. One rainy day I decided to take it upon myself to investigate why the trim indicator wasn't working and cranked the trip to it's stop not knowing this would jam the trim tab if the elevator wasn't in the neutral position. After reading several helpful post here by Robert Lees and many others I discovered my folly.
Due to the kind folks writing about their experiences I discovered that by loosening the tension on the trim cable that one could reset the trim tab to neutral by turning the pulley/jackscrew shaft at the rear.
I'm wondering if anyone could help a simpleton understand what is happening in that jack screw when this jam happens? I'm assuming the screw has reached its end? in this case its bottomed out and I'm assuming that if one where to have turned the trim wheel in the opposite direction the jack screw would have come out of the threaded portion of its carrier? Is that correct?
Lastly, why does this only happen when the horizontal stabilizer is out of the neutral position?? I understand that the travel is limited by the spring tensioner at the rear and the limiting bolt at the front of the trim wire but it makes me a little concerned for making large adjustments while in flight, like for slow flight/stall training.
Many thanks for your thoughts, this board is a great resource.
Comment