As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER FUSELAGE SKIN AT F.S. 288 AND STRINGER 1 IS CRACKED, CRACK RADIATES FORWARD FROM FASTENER .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-017. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.