Both of my aileron push pull tubes have corrosion on them. One is worse than the other. I seem to remember that 10 % of the thickness is the limit before it has to be replaced. Is that correct?
Both of my aileron push pull tubes have corrosion on them. One is worse than the other. I seem to remember that 10 % of the thickness is the limit before it has to be replaced. Is that correct?
They corroded under the aileron boot at the net entrance into the fuselage.