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 WITH AN AREA OF CORROSION AT FS 685 AT STRINGER 27L. THE CORROSION WAS REMOVED WITH A 4 X 5 INCH CUTOUT. THE CUTOUT WAS BETWEEN AN EXISTING DOUBLER REPAIR AT STRINGER 26L AND ANOTHER AT STRINGER 28L. THE EXISTING REPAIRS WERE REMOVED, THE SKIN INSPECTED FOR CRACKS AND ALL THREE AREAS REPAIRED WITH A SINGLE EXTERNAL REPAIR DOULBER PER ER/A 379004-14.