As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 PYLON LT SIDE SKIN EXFOLIATED AROUND FASTENERS APPROX BETWEEN P/P STA 136 AND 140, AND 1 INCH ABOVE LWR SPAR. CORROSION ON NR 2 PYLON SKIN FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS. PYLON SKIN REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSIFIED AS MAJOR IAW 6-2-100 CRITERIA.