What was found
DAMAGE TO THE RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACE OF THE FRAME. THE RH EDGE FRAME WAS PARTIALLY REPLACED AND SPLICED INTO THE REMAINING SERVICEABLE FRAME. 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.