As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LEADING EDGE 5 SLAT HAS CORROSION UNDER PANEL SS128. MECH REMOVED CORROSION AND TR WING LEADING EDGE SPAR IAW SRM 51-10-6. REMOVED AT .088 METAL ORIGINAL THICKNESS .360 MATERIAL ALLOWABLE .012 OUT OF LIMIT IAW SRM 57-10-1. NO CRACKS NOTED BY EDDY CURRENT. FLAP PEENED AREAS IAW B727 SOP 20-10-3. TREATED ADN PRIMED IAW SRM 51-10-2 AND MM 51-10-11.