As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .75 INCHES AND INSTALLED FILLER FABRICATED FROM 2024 T3 0.090 AND REPAIR DOUBLER FABRICATED FROM 2024 T3 0.100 IAW A300 SRM 53-10-10.