As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND 3 CRACKS RUNNING FROM FASTENER HOLES IN SECTION 41 SKIN PANEL ON RT SIDE OF FUSELAGE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE EXISTING DOUBLER WAS REMOVED AND THE DAMAGED SKIN WAS CUT OUT. FILLERS AND DOUBLERS WERE INSTALLED IAW SRM 53-30-2 AND SRM 51-30-2. (X)