As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON FUSELAGE FRAME LOWER FLANGE AT X 216.00, BETWEEN STR 30L AND STR 31L. CORROSION ON FUSELAGE FRAME LOWER FLANGE AT X 216.00 BETWEEN STR 30L AND STR 31L WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 REPAIR 9 REV 16. PERFORMED A LOOSE ANGLE REPAIR TO FUSELAGE FRAME LOWER FLANGE IAW SRM 53-00-00 REPAIR 18. NO CRACKS FOUND.