As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION- AFT WET AREA- RH STIFFENER BETWEEN FR 89 AND FR 90 AS MARKED. LOCATED DRILLED AND ALODINED NEW RH STIFFENER BETWEEN FR 89 AND FR 90 REF EMB SRM 51-40-02 SRM 51-23-04 INSTALLED RH STIFFENER BETWEEN FR 89 AND FR 90 REF EMB SRM 51-40-08 APPLIED TOPCOAT PO # 256614 REF SRM 51-23-06 APPLIED CIC TO RH STIFFENER REF CPM 51-25-00 SEE EAMS W/O H6415 SN 415 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.