As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH AND .375 INCH CRACK IN FUSELAGE SKIN AT STA 168, RBL 15 FORWARD OF R-1 SERVICE DOOR. THE INNER SKIN ACCESS PANEL FORWARD OF R-1 DOOR WAS REMOVED IAW SRM 51-30-1. THE CRACKED AREA WAS REMOVED. FILLER AND DOUBLER WERE INSTALLED IAW SKETCH DHSK233-507, SRM 51-30-2, AND 51-30-5. THE INNER SKIN ACCESS PANEL WAS REINSTALLED IAW SRM 51-30-1 AND ECRA 5330-02975.