As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL LOCATIONS BETWEEN BS 188-251.6 RIGHT SIDE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED SECTION OF SKIN WAS REMOVED. REPAIR DOUBLER S AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188 AND SRM 51-30-2. (W)