As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GSO - INSPECTION FOUND CRACKS AROUND FASTENERS IN LT EXTERNAL SKIN AT BS 188 TO BS 251, WL 207 THROUGH WL 234. THE CRACK LENGTHS WERE NOT IDENTIFIED, BUT THE REPAIRED AREAS WERE LESS THAN 6 INCHES IN DIAMETER. THE CRACKS WERE CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW E.A. 53-10-01188. (X)