What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00032) REF AE NR 2025-717375, WO 2025-414/1 - **FUR-A320-53-02840 CREATED ***, PERFORMED PERMANENT REPAIR ON HOLE A AT FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA IAW A320 SRM 53-11-12-300-012 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT 6800FC/FH NOT RELEVANT SUBSEQUENT INSPECTION AT 6800FC/FH NOT RELEVANT INTERVALS UNTIL 60000 FC/ FH NOT RELEVANT INSPECTION METHOD FOR LEADER AND ASSOCIATED HOLE ROTOTEST INSPECTION IAW A320 SRM 53-11-12-205-008 TABLE 1.