As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.