As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C CHECK FOUND EXTERIOR FUSELAGE 1/4/ INCH CRACK BETWEEN STA 1310-1320 L-11R TO L-12R. REMOVED FASTNERS WITHIN DAMAGED AREA PER SRM 51-1-21. TRIMMED OUT DAMAGED AREA PER SRM 53-2-1. TREATED AND PRIMED AREA PER SRM 51-1-8B. FABRICATED FILLER AND DOUBLER PER SRM 53-2-1. INSTALLED REPAIR PARTS PER SRM 51-1-20 AND 21.