What was found
DAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ACROSS THE ENTIRE LENGTH OF THE OUTBOARD FACE OF THE FRAME. THE LH EDGE FRAME 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.