What was found
OVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LOWER FRAME (P/N: 350A211245.22), AND MAINTENANCE STEP (P/N: 350A21137.20) DURING REMOVAL AND REPLACEMENT OF THE L/H MAINTENANCE STEP. THE DAMAGE CONSISTED OF OVERSIZED AND BLOWN OUT FASTENER HOLES, WITH THE LARGEST MEASURED AT 0.209.” THE LOCATION OF THIS DAMAGE IS LOCATED FROM F.S 4168MM TO 4340MM AND W.L -2066.4MM TO -2264.4MM4168. A DETAILED DESCRIPTION OF THE TYPICAL DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL RDAS-EC130-53-2025-3620A ISSUE A DATED 11 NOV 2025.