As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION DAMAGE WAS DISCOVERED ON THE LOWER FLANGE OF FRAME 1 WEB (PN: L533M1011211) ON THE LH AND RH SIDES. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-1990, ISSUE A DATED 26 JUN 2024.