As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE RH SIDE FRAME 4 INNER SKIN PANEL IS DAMAGED IN THE FORM OF TWO (2EA) CHAFE DAMAGE AREAS. THE FIRST CHAFE DAMAGE AREA IS REPORTED TO BE 1.75” X 0.6” IN SIZE AND 0.026” DEEP AT THE DEEPEST POINT. THE SECOND CHAFE DAMAGE AREA IS REPORTED TO BE 1.25” X 1.0” IN SIZE AND 0.016” DEEP AT THE DEEPEST POINT. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2025-3789, REV A DATED 23 NOV 2025.