As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 8 INCH BY 3 INCH CORRODED AREA ON BOTTOM AND SIDES OF STRINGER. STRINGER 27L BENEATH FRAME AT BS 967. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIR PER SRM 53-10-3 FIG 1. (M)