What was found
FWD FUSELAGE FR13+65MM AND 400MM ABOVE OF LEFT SIDE STRG SKIN PANEL WITH NICK. PERFORMED PERMANENT FUSELAGE SKIN REPAIR AT FWD FUSELAGE FROM FR 12 +238MM TO FR 13 +155MM, BETWEEN Z-520 AND Z-742 L/H SIDE I.A.W A320 SRM 53-11-11-300-041 PARAG 1 AND PARAG 2A FIGURE 001. NOTE: THIS REPAIR IS CATEGORY B REPAIR AND MUST BE INSPECTED I/ A/W TASK A320 SRM 53-11-11-205-037 PARAG 2 TABLE 001, INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT: 60000 FC / 120000 FH (WHICHEVER VALUE FC / FH OCCURS FIRST) SUBSEQUENT INSPECTION AT INTERVALS OF: TBD, INSPECTION METHOD: TBD, TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60000 FC / 120000 FH (WICHEVER OCCURS FIRST), A320 SRM REV 158.00 DATED 01-JUN-26. (LP: 1690852, AIRCRAFT WAS GROUNDED)