What was found
LT WING I/B FLAP UPPER SKIN HAS A CRACK NEAR O/B END. CLEANED AREA IAW M/M 12-22-02-7, HFEC INSP PER NTM 51-00-00 CRACK FOUND 3 EA. REMOVED T/E SECTION IAW SRM 51-31-01. REMOVED DAMAGED AREA IAW SRM 57-10-00, FIG 85. FAB DOUBLER AND FILLER MAT THICKNESS 2024 T3 040 BATCH 1011107. LOCATED AND DRILLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85. INSTALLED ASSY PARTS IAW SRM 51-31-01. REINSTALLED T/E WEDGE IAW SRM 51-31-01. PREP AND PAINTED LT WING I/B FLAP UPPER O/B IAW SRM 51-21-02.