What was found
CORROSION AT, AFT PIT, R/H FRAME C51, STRINGER 38 LATE FIND GROUNDED - YES. REMOVED CORROSION AND CHECKED THE LIMITS. ORIGINAL THICKNESS IS .095, REMAINING IS .083, .012 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11 AND AIRBUS DWG E53470525 ISSUE K. REPAIRED STRINGER 38R REF ASA EA A320-53EA-00361 REV"00" AND A320 SRM 53-00-13-300-001. THIS IS A CATEGORY "A" REPAIR.