What was found
DURING INSPECTION, FOUND 3 AREAS OF CORROSION ON FUSELAGE SKIN BETWEEN S26R AND S27R FRAME 58 - 60. REPAIRED PER AVBORNE REPAIR REF 25599-3-01-18-06, (AIRBUS REPAIR DESIGN APPROVAL SHEET RAS/DAHM/40204/2006) REMOVE FASTENERS, SMOOTH BLEND CORROSION, HFEC AND ROTO-TEST TO CONFIRM AREA IS DAMAGE FREE, FLAP PEEN PER SRM 51-40-19 REINSTALL FASTENERS AND RESTORE SURFACE PROTECTION PER SRM 51-40-12.