What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16 RH SIDE AT HOLE A. CRACK DIRECTION 9 OCLOCK (VIEW FROM OUTSIDE) AND CRACK LENGTH 0.100 INCHES (1EA); PERFORMED PERMANENT REPAIR LOC. ON DOUBLE JOGGLE AREA HOLE A ON FR16 RH SIDE IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CATEGORY B AND INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 6800 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT OF 5900 FC (FH NOT RELEVANT), INSPECTION METHOD FOR LEADER HOLE REFER TO TASK 53-11-12-300-12 FIGURE 014: FUR-A320-53-02031