What was found
DURING INSPECTION, THE COCKPIT FLOOR UPPER SHEET (PN: B531M8020201) AND LOWER SHEET (PN: B531M8021201) ARE DAMAGED IN THE FORM OF CORROSION AT THE LOCATIONS OF THE FWD GROUNDING POINTS. THE CORROSION AREAS FOR THE UPPER SHEET WERE MEASURED TO BE APPROXIMATELY 1.0” X 1.0”. THE CORROSION AREA FOR THE LOWER SHEET WAS MEASURED TO BE APPROXIMATELY 1.0” X 0.50”. DESCRIPTION OF WORK: REPAIRED THE DAMAGE IN ACCORDANCE WITH AIRBUS REPAIR DESIGN APPROVAL RDAS-BK117-53-2022-0123 ISSUE A DATED 20 JAN 2022. APPROVED DATA: RDAS-BK117-53-2022-0123 ISSUE A DATED 20 JAN 2022 IS EASA APPROVED (DOA EASA.21J.700). IAW THE FAA AND EASA BILATERAL AGREEMENT AND TECHNICAL IMPLEMENTATION PROCEDURES, THE FAA CONSIDERS THE DATA FAA APPROVED.