As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE TO THE LH KEEL BEAM CAP IN THE FORM OF SEVERAL AREAS OF CORROSION WAS DISCOVERED. THE DAMAGE IS LOCATED ON THE UPPER SURFACE OF THE PART UNDER THE COCKPIT FLOOR, WITH THE LARGEST DAMAGE AREA REPORTED TO BE APPROXIMATELY 0.5” X 0.5” IN SIZE AND 0.018” DEEP. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2026-3337, ISSUE A DATED 21 SEP 2026.