As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE RHS FUSELAGE SKIN WAS FOUND WITH AN APPROX 2 INCH LONG CRACK AT WL 146, JUST FORWARD OF FS 983 AND ABOVE STRINGER 21, THE CRACK EXTENDS HORIZONTALLY THROUGH TWO FASTENER HOLES. ANOTHER 1 INCH LONG CRACK WAS FOUND IN THE HORIZ FLANGE OF THE BULKHEAD CAP, EMANATING HORIZ FWD AND AFT OF THE AFT MOST FASTENER. THE CRACKS ARE THE SUBJECT OF LAC S/B 093-53-273, AND DAL SI 7-69018-12 WHICH MANDATES INSPECTION OF THE LONGERON, SKIN AND CAP.