What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD SIDE OF THE FORWARD PRESSURE BULKHEAD AT -Z180 AND +Y1000. REPAIR WAS ACCOMPLISHED PER AVBORNE REPAIR REF: 25599-10-01-25-06, (AIRBUS TECHNICAL DISPOSITION 942.042586/004/2006) SMOOTH REWORK OF CORRODED AREA, VERIFY CORROSION REMOVAL PER NTM 51-30-11, PERFORMED HFEC PER NTM 51-31-05 TO ENSURE HOLE AND SKIN ARE DAMAGE FREE. MANUFACTURED AND INSTALLED SHIM AND DOUBLER PER PAGE 4 - 5 OF REPAIR REFERENCE 25599-10-01-15-06.