Hi all
A new FNG here to the forum looking for input on rebuilding an old set of wings with new wooden spars from Rainbow Flying Services. Through the over head inspection plates a compression fracture was found on the right (starboard) wing after the backing plate. Spoke with “Ron” from Rainbow Flying Service and he said it was probably caused by excessive loading to the wing from an aerial maneuvers gone bad. I don’t own a chute and haven’t participated in any aerobatics in this bird but I have literally cheated death in the 19 hours I’ve flown in this airplane before finding this fracture on a annual inspection. If it were not for Ron’s STC for the square inspection plates on top of the wing we would have never found this crack.
Anyway, I am a A&P with a good set of tools and a nice hanger to work in. I have a good understanding of wood working but not on wooden aircraft. I have worked with the Polyfiber process and comfortable with its application though I have never recovered an entire wing. Besides removing the fabric and the tedious process of removing the nails from the old spar. How difficult is it get the old spar out and the new spar back in and re-attached. Is it best to start with main spar then the rear spar or vice versa. Besides the AC43-13 is there other guidelines or videos I can reference?
Thanks for reading..
A new FNG here to the forum looking for input on rebuilding an old set of wings with new wooden spars from Rainbow Flying Services. Through the over head inspection plates a compression fracture was found on the right (starboard) wing after the backing plate. Spoke with “Ron” from Rainbow Flying Service and he said it was probably caused by excessive loading to the wing from an aerial maneuvers gone bad. I don’t own a chute and haven’t participated in any aerobatics in this bird but I have literally cheated death in the 19 hours I’ve flown in this airplane before finding this fracture on a annual inspection. If it were not for Ron’s STC for the square inspection plates on top of the wing we would have never found this crack.
Anyway, I am a A&P with a good set of tools and a nice hanger to work in. I have a good understanding of wood working but not on wooden aircraft. I have worked with the Polyfiber process and comfortable with its application though I have never recovered an entire wing. Besides removing the fabric and the tedious process of removing the nails from the old spar. How difficult is it get the old spar out and the new spar back in and re-attached. Is it best to start with main spar then the rear spar or vice versa. Besides the AC43-13 is there other guidelines or videos I can reference?
Thanks for reading..


