Ok thanks for the comments!
The main corrosion in question, from what I have seen, is located on the underside of the wing in a small area around the front attachment bolts, and some on a flap bracket and a bit more on one of the fuselage strakes. Interestingly on the other wing a new plate had been affixed in the same area (around the attachement bolts).
Regarding structural corrosion, to be 100% sure there isn't any - this would require a full survey I assume, as the inspection I had done only highlighted the surface occurances?
Should a CoFA pickup any structural corrosion?
Thanks again.
Last edited by XX621; 4th April 2008 at 10:37.