What was found
LEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT<[01] REMOVED LEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ANGLE PER DWG#115A6200 REV A AND 51-40 05 OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2 OK TO INSTALL;[04] INSTALLED NEW ANGLE PER DWG#115A6200 REV A AND 51-40 05;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] TASK CARD COMPLETE.