As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK AT LEFT SIDE OF FUSELAGE AT CUTOUT FOR L-1 DOOR UPPER HINGE ARM. THE CRACKED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5330-02675, SRM 51-10-2 AND SRM 51-30-2, AND SERVICE BULLETIN 727-53-0198.