What was found
RIGHT WING O/B AFT FLAP HAS A DELAM ON I/B LOWER CORNER / DELAMINATION I/B LOWER CORNER UPPER SKIN . 8'X2' EXCEEDS ALLOWABLE LIMITS AS GIVEN IN SRM 57-53-01-1A-1 PARA 4 . A. (5) APPLY A PERMANENT REPAIR IAW SRM 57-53-01-2R-4 PARA 1. A. PARA 3. A. & B . PER SRM 51-70-10-2R-10 .ALIDATED REPAIR PER IAW SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-0;[08] FABRICATED THE REPAIR DOUBLER AND FILLER FROM PRE-PRIMED 0.16' 7075 T6 ALUMINUM (LOT# 1351319-2) ACCORDING TO SRM 51-70-10-2R-0; PARA'S 8.A. AND 10.A.PREPARED REPAIR AREA FOR BONDING USING BMS 5-162 (BOEGEL) SURFACE TREATMENT (LOT#2018E) AND BMS 5-89; TY2 (LOT# 5110236-1) ALL ACCORDING TO SRM 51-70-10-2R-0; PARA'S 14; 15.A THRU 15.E.(2).; 15.F THRU 15.H.(1).(A)<BR><BR>APPLIED REPAIR PARTS TO THE REPAIR AREA USING BMS 5-101; GR 10 ADHESIVE (LOT# 1484596-1); AND BMS 5-121 POSITIONING FABRIC (LOT# 582593-1); VACUUM BAGGED REPAIR AREA FOR HEAT BLANKET CURE; ACCOMPLISHED VACUUM BLEED DOWN TEST (PASS); THEN CURED REPAIR AREA; ALL ACCORDING TO SRM 51-70-10-2R-0; PARA'S 18; AND 20.B.<BR><BR>REMOVED ADHESIVE FLASH; THEN ACCOMPLISHED VISUAL EXAMINATION AND TAP TEST (NO DISBONDS NOTED); ALL ACCORDING TO SRM 51-70-10-2R-0; PARA. 21. CLEANED THE REPAIR AREA AND SEALED THE EDGE OF THE DOUBLER USING BMS 5-95 SEALANT (LOT# 45101031F-14); ALL ACCORDING TO SRM 51-70-10-2R-0; PARA'S 22.A AND 22.B.;REFINISHED REPAIR AREA ACCORDING TO SRM 51-70-10-2R-0; PARA. 22.C; AND AMM 51-21-99-300-802; PARA. 3.C.(3