What was found
DAMAGE TO THE AFT MAIN LANDING GEAR FITTING AREA WAS FOUND IN 2 LOCATIONS. CHAFE DAMAGE WAS FOUND ON A PREVIOUSLY INSTALLED “AFT LANDING GEAR CROSS BEAM REPAIR BLOCK” (P/N RDAS AHI 130 53 005 24.01) IN THE FORM OF CHAFING. DAMAGE WAS ALSO FOUND ON THE AFT LANDING GEAR CROSS BEAM (P/N 350A214311.20) IN THE FORM OF CHAFING. A NEW REPAIR BLOCK (P/N: RDAS-EC130-53-2025-2585.01) WAS FABRICATED, USING 17-4 PH, H1025 1.5” PLATE, AND INSTALLED. ALL DAMAGE TO THE AFT LANDING GEAR CROSS BEAM WAS BURNISHED TO A SMOOTH CONTOUR. A DETAILED DESCRIPTION OF THE DAMAGE AND THE APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2025-2585 A, ISSUE A DATED 22 AUG 2025.