As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(A204 DOT 2) LH WING; DEFLECTION CONTROL RIB UPPER TAB IS WORN AT BOLT HOLES LOCATIONS WITH EVIDENCE OF CRACKING AT AFT FASTNER; JUST BELOW BOLT.<[01] REMOVED DAMAGE FROM LH WING; DEFLECTION CONTROL RIB UPPER TAB AND REPAIRED PER SRM 57-51-02-2R-4;[02] COMPLETE <BR>AUDIT C/W