As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND SEVERAL FASTENER HOLES CRACKED IN RT FUSELAGE SKIN AT BS 188 TO 251 BETWEEN WL 207 AND WL 234. THE CRACKS WERE ALL APPROXIMATELY .1 INCH LONG. THE CRACKED SKIN SECTIONS WERE CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-01188. (W)