What was found
TAIL CONE ACCESS PANEL NUMBER 317AL INTERNAL ANGLES WITH CORROSION. REPLACED TAIL CONE ACCESS PANEL 317AL INTERNAL ANGLES (2EA) IAW SRM 51-72-11-911-001 PARAG 2C REV 155, AND AIPC 53-58-04-05B SHEET 1 & 2 DETAIL H & J, REV 133.01, AND AIRBUS REFERENCE DWG D924 85120 ISSUE R. (LP: 1401822)