What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE IN OPEN FASTENER HOLE H6 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, AT FWD GALL EY AREA (2 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00041) PERFORMED PERMANENT REPAIR LOCATED ON DOOR FRAME 20 RH AT UPPER DOUBLE JOGGLE AREA ON HOLE 6 IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CATEGORY B. INSPECTION OF REPAIR IAW SRI 53-11-12-205-008, TABLE 002 ARE: INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN AT 60000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT AT 4700 FC (FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01 AND NTM 51-10-18. INSPECTION METHOD FOR ASSOCIATED HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01.WORK ACCOMPLISHED ON AEROMAN WO:2023 365/1 NRC: 2023-768517 FUR-A320-53-01159.