As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON INNER STRUCTURE BETWEEN FRAME 13 AND 17 RT STRINGER. CORROSION REMOVED ON INNER STRUCTURE BTN FR 13 AND 17 RT STRINGER 14 IAW SRM 51-21-42. INNER STRUCTURE BETWEEN FR 13 AND 17 RT STRGR 14 REPAIRED IAW SRM 53-31-50 FIG 402 COMPLIED WITH EC/TC EO 72-53-0236 MATERIAL THICKNESS 0.071 MATERIAL REMOVED 0.032 WITHIN LIMITS AS PER SRM 53-31-00 FIG 301 ASA RII C/W. (CLOSED)