What was found
DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND LEFT WING SKIN FORWARD OF FRONT SPAR OLES 1378-1387, 1410, 1438-1447. CORROSION WAS REMOVED BY BLENDING. NDT INSPECTED TO CONFIRM DAMAGE FREE CONDITION. BLENDED AREAS WERE FLAP PEENED, ALODINE 1200 AND BMS 10-11 TYPE II PRIMER APPLIED. CUSTOM FILLERS WRE INSTALLED. TO RMOVED CORROSION AT OLES 1410, THE EXISTING CUTOUT IN THE SKIN LOCATED 4 INCHES OUTBOARD IS ENLARGED. SKIN FILLER IS SEGMENTED SO AS NOT TO BE LONGER THAN 8 INCHES. THREE REPAIR PLATES WRE MADE FROM .096 INCH THICK 2024-T3 ALUMINUM. (M)