As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE MAIN CABIN STA 1110 BETWEEN RBL 15 AND LBL 63 FLOORBEAM UPPER CHORD WITH CORROSION SEVERAL PLACES. REPAIRED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1110 FROM LBL 13.750 TO RBL 70 IAW EO COO-2-53-272-08 DTD 9/14/08 DOCUMENTED ON FAA FORM 8110-3.