As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION: CUSP ANGLE AT STA Y-200 ON STRINGER L18 WAS REPAIRED PER B717-200 SRM 53-00-55-2 REPAIR 3 PAR. 5. (LP 2689728)