What was found
(AIRCRAFT 6716, L/P 1310641) DURING INSPECTION, 02 DISBONDED AREAS WERE FOUND. 01 TO 3 IN FROM THE INBOARD EDGE ( 3.5 IN X 1.5 IN ) AND THE OTHER TO 91 IN FROM THE INBOARD EDGE, ON PREVIOUSLY REPAIR ( 2.375 IN X 1.750 IN ) ON SLAT 5 UPPER SKIN. CORRECTIVE ACTION: CHANGED TO A/C 6716 PER FTN 8X97A6. DISBONDED AREAS WERE FOUND. 01 TO 3 IN FROM THE INBOARD EDGE ( 3.5 IN X 1.5 IN ) AND THE OTHER TO 91 IN THE INBOARD EDGE, ON PREVIOUSLY REPAIR ( 2.375 IN X 1.750 IN ) ON SLAT 5 P/N: 114N3002-131A S/N: A1-812 UPPER SKIN. WERE REPAIRED PER B757-200 SRM 57-43-02 REPAIR 1 AND B757-200 SRM 51-70-10 REPAIR GENERAL. REPAIR CLASS 3 AND WEDGE TYPE "A": PERFORM A DETAILED VISUAL INSPECTION WITHIN 600 TRAILING EDGE WEDGE FLIGHT CYCLES OR WITHIN 6 MONTHS (WHICHEVER OCCURS FIRST) PER B757-200 SRM 57-43-02 REPAIR 1 NOTE: E AND SB 757-57-0066. CHANGED FROM L/L TO REP PER 757 SRM 57-43-02 REP 1 PAGE 205, NOTE 4.