As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(A204 DOT 7) RH WING TRAILING EDGE; JUST INBOARD OF DEFLECTION CONTROL RIB. FIXED TRAILING EDGE PANEL; LATTERAL SUPPORT ANGLE IS CRACKED AT OUTBOARD FASTNER HOLE COMMON TO PANEL.<[01] REMOVED AND REPLACED R/WING T/E; FIXED PNL LATTERAL SUPPORT ANGLE IAW 51-40-02. AND DWG # 115A2156 REV E.;[02] VERIFIED ITEM 1