As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(A204 DOT 3) RH WING TRAILING EDGE CAVITY. 1 INCH INBOARD OF DEFLECTION CONTROL RIB. AND 24 INCHES FWD OF PANEL TRAILING EDGE. LATTERAL SUPPORT ANGLE IS CRACKED OUTBOARD FASTNER HOLE COMMON TO SKIN.<[01] REMOVED AND REPLACED LATTERAL SUPPORT ANGLE ON RH WING T/E CAVITY. 1 INCH I/B OF DEFLECTION CONTROL RIB. AND 24 INCH FWD OF PANEL T/E I.A.W. DWG 115A2512 AND SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>C/W