What was found
L/W O/B AFT FLAP LOWER SURFACE SKIN DELAMINATED 25' FROM O/B END<[01] IDENTIFIED L/W O/B AFT FLAP IAW SRM 57-53-01-0I-4 FIGURE 2 TABLE 2 ITEM 5 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-5 PAR.4 A(3)<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 57-53-01-2R-14.<BR><BR>REMOVED DAMAGE TO THE LOWER SURFACE SKIN MEASURING 2'X0.5'; WITH NO DAMAGE NOTED TO THE HONEYCOMB CORE OR TRAILING EDGE FILLER IAW SRM 57-53-01-2R-14 PAR.4 B & SRM 51-70-10-2R-0 PAR.6-7;[02] VALIDATED APPLICABILITY OF DAMAGE TO BE REPAIRED IAW SRM 57-53-01-2R-14 AND SRM 51-70-10-2R-4.;[03] VERIFIED CORRECTIVE ACTION ITEM 1-2.;[04] FABRICATED LOWER SKIN T/E FILLER AND REPAIR DOUBLER USING 7075-T6 0.020: LOT#1470922-1 IAW SRM 57-53-01-2R-14 PAR.4 C-D & SRM 51-70-10-0G-0 PAR.8 A<BR><BR>COMPLETED SURFACE PREP OF TRAILING EDGE FILLER LOWER SURFACE USING BOEGEL PROCEDURE (AC-130-2 LOT #2122E); AND APPLIED & CURED BONDING PRIMER (BMS 5-89 TYII LOT #1513769-1) IAW SRM 51-70-10-0G-0 PARA 14 & 15.;[05] INSTALLED LOWER SKIN FILLER & REPAIR DOUBLER USING ADHESIVE EA9696 LOT#1515859-1; AND BMS5-121 POSITIONING FABRIC;8[09] L/W O/B AFT FLAP LOWER SURFACE DELAMINATION WAS REPAIRED IAW SRM 57-53-01-2R-14 & SRM 51-70-10-2R-4;[10] FINAL INSPECTION. JOB COMLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.