What was found
LT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON UPPER SURFACE NEAR I/B AFT CORNER.<[01] IDENTIFIED AFT FLAP IAW SRM 57-53-01-0I-4; FIG 2; TABLE 2; ITEM 2.<BR><BR>DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-4 PARA 4.A (5).<BR><BR>DAMAGE IS REPAIRABLE IAW SRM 51-70-10-2R-4 AS DIRECTED BY SRM 57-53-01-2R-4 PARA 3.B.<BR><BR>STARTED DAMAGE REMOVAL OF UPPER SKIN (APPROX 10' X 10') IAW SRM 51-70-10-2R-4 PARA 3.A.;[02] FLAP ASSEMBLY WILL BE REMOVED AND REINSTALLED ON TTG8Q00L4LDF.;[03] UPDATED PARTS REQUIREMENT;[04] /LT WING O/B AFT FLAP WAS REPLACED AND WILL BE REMOVED AND INSTALLED ON THE AIRCRAFT ON FAULT TTG8Q00L4LDF.;[05] VERIFIED CORRECTIVE ACTION STEPS 1-4. TASK CARD COMPLETE.