As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT TUNNEL AREA AT BS 365 NLG WW WALL STIFFENER HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. CHECK LIMIT ORIGINAL MATERIAL .120 MATERIAL LOSS .039. FOUND OUT OF LIMITS IAW SRM 53-10-14 FIG 101 DETAIL II. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02 AND DWG 141N9951. MAJOR REPAIR.