What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 6, CRACK DIRECTION AT 11 O CLOCK LOOKING INBOARD, D=0.125 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00033) REF AE NR 717377, WO 2025-414/1 - ***FUR-A320-53-02841 CREATED ***, PERFORMED PERMANENT REPAIR ON HOLE 6 AT FRAME 20 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 8900FC/FH NOT RELEVANT, SUBSEQUENT INSPECTION AT 8900 FC/FH NOT RELEVANT INTERVALS UNTIL 60,000 FC/ FH NOT RELEVANT INSPECTION. METHOD FOR LEADER AND ASSOCIATED HOLE ROTOTEST INSPECTION IAW A320 SRM 53-11-12-205-008 TABLE 2.