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 ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE SKIN AT FS 150 & STRINGER 9AL AT THE LOWER SNUBBER MOUNT AND AS DOOR FUSELAGE FRAME CRACKED AT SNUBBER UP MOUNT NUTPLATE AREA, BOTH 1.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-036 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.