As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
KUL - C-CHECK - CORROSION FOUND AT RT WING SPAR STIFFENER OF FRONT SPAR NR 2 FROM WS 251 (NR 5 KRUGER FLAP AREA). CORROSION REMOVED AND FOUND BEYOND LIMIT IAW SRM 57-10-1 AREA 3 INCHES BY 1.5 INCHES BY 0.024 INCH. STIFFENER REPLACED IAW SRM 51-30-2. HYDRAULIC PIPING AND BONDING REINSTALLED. FOR FUEL LEAK CHECK OF FASTENERS REFER HNRC 869988. (X)