What was found
DAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22) AND RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. BOTH LH AND RH EDGE FRAMES REQUIRED FULL REPLACEMENT. THEREFORE, CUTS OR SPLICING DOUBLERS WERE NOT REQUIRED. A DETAILED DESCRIPTION OF THE APPROVED REPAIR/INSTALLATION PROCEDURES IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2024-0040, ISSUE A DATED 09 JAN 2024, AND AC 43.13-1B CHAPTER 4, SECTION 4, PARAGRAPH 4-57 CHANGE 1 DATED 9/8/98.