As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - NEAR THE FWD AIRSTAIR DOOR CUTOUT AT THE LOWER FWD CORNER, FUSELAGE EXTERIOR SKIN AT FS 150 AND STRINGER 11L WAS FOUND CRACKED AT A RIVET HOLE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-53-015, STEPS 9-14. MATERIALS UTILIZED ARE INCLUDED IN THE EO.