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 A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-052. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.