What was found
DURING HEAVY MAINTENANCE: CRACK: HOLE 5 FR16R UPPER DOUBLE JOGGLE AREA AT NOSE FWD FUSELAGE. D= 0.050"@ 5 O'CLOCK LOOKING FROM OUTSIDE; (RESOLVED ON W/O: 1330742 TASKCARD: NR-00020) REF AEROMAN 2025-168992 W/O:2025 82/1: PERFORMED PERMANENT REPAIR ON HOLE #5, LOCATED ON FR 16 RH SIDE UPPER DOUBLE JOGGLE AREA DOOR IAW A320 SRM 53-11-12-300-012, FIGURE 012 (SHEET 1). THIS REPAIR IS CATEGORY B. INSPECTION OF REPAIR IAW SRM 53-11-12-205-008, INSPECTION THRESHOLD FROM TIME OF ADL/ REPAIR EMBODIMENT AT 6800 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC/FH NOT RELEVANT 6800 FC (FH NOT RELEVANT), INSPECTION METHOD FOR LEAD HOLE AND ASSOCIATED HOLE REFER TO TASK 53-11-12-300-012 FIGURE 013: FLOWCHART FOR REPETITIVE INSPECTION. FUR-A320-53-02145 CREATED.