As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT FUSELAGE STA 907 AT STR 27L AT STRINGER SPLICE. REMOVED STRINGER SPLICE AND STRINGER CLIP DUE TO CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. FABRICATED REPAIR COMPONENTS IAW SRM 53-10-03. INSTALLED REPAIR COMPONENTS IAW SRM 51-30-02.