What was found
CHAFE DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK SUPPORT BEAM AFT SPLICE PLATE (PN: B533K3265-201) AT FS 4,963, MID SPLICE PLATE (PN: B533K3193-201) AND LH SUPPORT BEAM CAP (PN: B533K3202-201) AT FS 4,615, AND ON THE FORWARD SPLICE PLATE (PN: B533K3192-201) AND LH SUPPORT BEAM CAP (PN: B533K3202-201) AT FS 4,373. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2025-0989, ISSUE B DATED 10 APR 2025, WHICH CONTAINS A DETAILED DESCRIPTION OF THE DAMAGE AND REPAIR INSTRUCTION.