As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CIRCUMFERENTIAL SPLICE JOINT AT FS 280 INNER SKIN CORRODED BETWEEN STR 24LT-24RT. REMOVED CORROSION AT FS 280 BETWEEN STR 27-26R AND BETWEEN STR 25R-24R IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FROM FS 280, ST 26L-25L AND STR 26R-25R IAW SRM 51-21-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.