What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION OF FRAME 68 AT AFT GALLEY AREA (CRACK INDICATION FROM HOLE 2 OF FRAME 68LH OF DOOR STOP FITTING 1 AT AFT GALLEY AREA. CRACK DEPTH IS 0.096 INCH AND CRACK DIRECTION IS 12 O'CLOCK; REF AEROMAN WO# 2023-272/1 NR# 2023-424813 FOR WORK PERFORMED; PERFORMED REPAIR HOLE 2 LOC ON FR68 LH DOOR STOP FITTING 1. IAW A320 SRM 53-41-12-300-010 THIS REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 24,500 FH NOT RELEVANT. SUBSEQUENT INSPECTION AT INTERVALS FC 10.700 GH NOT RELEVANT. INSPECTION METHOD HFEC REFER TO NTM CHAPTER 51-10-08. AND ROTO TEST REFER TO AMM 53-41-00-220-813.IAW A320 SRI 53-41-12-205-009 TABLE 002 TABLE 002. FUR-A320-53-00846 CREATED.