As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** AT FWD END OF STRINGER SPLICE AT FASTENER; BS 353; STR 28 R / REMOVED CORROSION ON STRINGER SPLICE IN A AREA OF .5' X .5' X .020' ORIGINAL THICKNESS .028' FOUND TO BE OUT OF LIMIT PER SRM 53-00-03-1A-1 REMOVED AND REPLACED STRINGER SPLICE PER:SRM 51-40-02 AND DRAWING 141A3531