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 THREE AREAS OF CORROSION BETWEEN FS 1745 AND 1776 BETWEEN S-31 AND 33. THE CORROSION REMOVAL RESULTED IN THREE CUTOUTS SIZED 6 X 5, 5 X 4 AND 2 X 2. THE SKIN CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER AND TRIPLER REPAIR PER ER/A 365961-14, REV A.