As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FS 680 BUTT SPLICE BETWEEN STRINGER 28L AND 28R. AN EXISTING LOCAL REPAIR WAS REMOVED AT THIS LOCATION AND ALL CORROSION AREAS WERE CUT OUT OF THE SKIN WITH A 1 X 3 CUTOUT AND A 10 X 5 CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL REPAIR DOUBLER PER ER/A 366900-14, REV A.