As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND SEVERAL CRACKS IN SECTION 41 FUSELAGE SKIN ON LT SIDE, BS 188 TO 251, WL 207 TO 234. THE CRACKS RANGED FROM .125 INCH TO .25 INCH IN LENGTH. THE CRACKED AREAS WERE CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188 AND SRM 51-30-2.