What was found
RT WING O/B FOREFLAP HAS DELAMINATION DAMAGE. REMOVED DELAMINATED AREA APPROX 4.8" BY 2". CLEANED AND PREPPED REPAIR AREA TO BOND IAW B727 SRM 51-40-20 PAR 7 FIG 3. FABRICATED LOWER FILLER AND DOUBLER FROM .016" 2024T3 PO NR 9003189, REPAIR CORE FROM HRP-3/16-40-.5 PO NR 6348114 AND UPPER DOUBLER FROM .016 7075T6 PO 9003989 ANODIZED AND PRIMED REPAIR PARTS AND AREA TO BE REPAIRED IAW B727 SRM 51-40-20 PAR 8, 9, 14, 15 AND 51-40-24 FIG 2. INSTALLED ADHESIVE FILM AND CORE SPLICE ADHESIVE. INSTALLED REPAIR PARTS AND CURED REPAIR (IN TWO STAGE CURE) IAW B727 SRM 51-40-20 PAR 18, 19, 20 AND 51-40-24 FIG 2. FINISHED REPAIR AREA IAW B727 SRM 51-40-20 PAR 22 AND AMM 51-20-00. DIM OF REPAIR IS FILLER 2" BY 4.8" D