What was found
DURING C-1 CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE FROM XFS 11.25 TO XFS 182.5 HAVE CORROSION AROUND ATTACH FASTENERS AS MARKED. INSTALLED DOUBLER REPAIR IAW AIA SKETCH NR 2425, EA 96-348 REPORT NR 96-197 DATED 12-12-96. CORROSION CARD NR 121R-0552. NON-ROUTINE TASK CARD NR 91475, LEVEL 2.