As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSP FOUND A CRACK IN THE FUSELAGE FRAME DOUBLER AT BS 177.35 AND STRINGER 13L 1.2 INCHES FROM OTBD EDGE RADIATING INBD, CRACK IS IN THE FLANGE BEND RADIUS OF THE DOUBLER. REPAIRED IAW EO 13-1900-53-064. MAJOR REPAIR.