What was found
(A204 DOT 4) RH WING TRAILING EDGE CAVITY; 24 INCHES FORWARD OF PANEL TRAILING EDGE. ATTACH ANGLE COMMON TO DEFLECTION CONTROL RIB IS CRACKED AT LOWER OUTBOARD HOLE.<[01] 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[03] VERIFIED STEP 2<BR>AUDIT CW