As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING REMOVAL OF THE RT LWR AFT BODY FAIRING, ZONE 198, A CRACK WAS DISCOVERED IN THE FUSELAGE SKIN BETWEEN BS 1197 AND 1199, .5 INCH ABOVE STRINGER S-32R. THE CRACK IS APPROXIMATELY 1.625 INCHES IN LENGTH AND RUNS PARALLEL TO THE STRINGER. THE CRACK IS A RESULT OF LOCAL, LEVEL 2 CORROSION BEHIND THE AFT CARGO BIN SIDEWALL.