What was found
DURING INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN ABOVE THE RT FORWARD PASSENGER DOOR, TWO AREAS, AT S9L BETWEEN FR 14C AND FR 14B AND 1 AREA AT S11L BETWEEN FR13 AND FR13A. ACCOMPLISHED REPAIR PER AVBORNE REPAIR REFERENCE 25599-7-02-02-2006, (AIRBUS REPAIR DESIGN APPROVAL SHEET RAS/AS/028/2006) PERFORMED SMOOTH REWORK OF CORRODED AREAS, PERFORMED INSPECTIONS, ROTOTEST AND DVI OF HOLES IN CORRODED AREAS, HFEC AND DVI OF CORRODED AREAS, INSTALLED OVERSIZE FASTENERS IN CORRODED AREAS AND RE-PROTECT PER SRM.