As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT SIDEWALL FUSELAGE FRAME AT FS 107 AND JUCTION WITH LONGERON IN THE FRAME BEND RADIUS AT THE UPPER AND OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-038. MAJOR REPAIR.