What was found
LOWER EXTERNAL FUSELAGE AT FR 25+160MM, STGR 40L SKIN WITH TOOL MARKS. FOUND DURING PROCESS WITH ORNRC 100-269. REPAIRED LOWER FUSELAGE SKIN PANEL FROM FR25 +66.5MM TO FR25 + 296.6MM BETWEEN STRG 39LH-41LH DUE TO TOOL MARK OUT LIMITS I/A/W A319 SRM 53-21-11-300-090 FIGURE 001. REV.155.00 DATED 17-NOV- 26. NOTE: THIS IS CATEGORY B REPAIR WITH NSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 60 000 / FH 120 000 SUBSEQUENT INSPECTION UNTIL 60 000 FC / 120 000 FH AT INTERVALS OF FC TBD/FH TBD INSPECTION METHOD TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60 000 FC / 120 000 FH IAW SRM 53-21- 11-205-071 PARG 2.A TABLE 002 ZONE A FIG. 001. REV 155.00 DATED 17-NOV-26. (LP: 1520616) AIRCRAFT WAS GROUNDED.