As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE WAS DISCOVERED ON THE LH AND RH FRAME 5 AND INBOARD ANGLE AT THE UPPER AND LOWER ATTACH POINTS OF THE MEDICAL INTERIOR BEAM. THE CRACK DAMAGES DISCOVERED WERE LESS THAN 2.5” IN LENGTH. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2025-1104, ISSUE A DATED 28 MAR 2025, WHICH CONTAINS A DESCRIPTION OF THE TYPE OF DAMAGE OBSERVED AND REPAIR INSTRUCTION.