What was found
DURING A 1000 HR. INSPECTION, THE COCKPIT FLOOR UPPER SKIN PANEL WAS FOUND DAMAGED IN THE FORM OF MULTIPLE DENTS AND AREAS OF CORROSION. THE LARGEST DENT DAMAGE AREA IS REPORTED TO BE APPROXIMATELY 3.25” X 3.0” IN SIZE AND 0.025” DEEP AT THE DEEPEST POINT. THE CORROSION DAMAGE AREAS ARE LOCATED AROUND THE CENTER POST OPENING WITH THE LARGEST CORROSION DAMAGE AREA BEING APPROXIMATELY 2.5” X 1.4” IN SIZE. 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.