As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION, FOUND FUSELAGE FRAME AT BS 1110 WITH LEVEL 2 CORROSION AND HOLE DAMAGED IN UPPER SECTION BETWEEN STRINGER 27L AND STRINGER 29L. REPAIRED FUSELAGE FRAME UPPER SECTION AT BS 1110 BETWEEN STRINGER 25L AND 27L IAW SRM 51-40-3. (M)