As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CRACKED AT L2 DOOR CUT OUT AT FWD LWR CORNER EMANATING FROM FASTENER AND RUNNING TO EDGE OF RADIUS. STOP DRILLED CRACK; CUT OUT ADJACENT DENTED AREA; FABBED REPAIR DOUBLERS AND FILLER; TREATED AND INSTALLED IAW AWA ER 03-5330-0-1052-SS1 AND SRM 53-60-01, 51-20-01 AND 51-40-02.