As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE FUSELAGE SKIN AT STA 303.9 BETWEEN STR 10 AND STR 14 WAS CRACKED AT THE LOWER FORWARD CORNER OF THE FORWARD ENTRY DOORWAY (L-1) LOWER HINGE CUTOUT. THE CRACK MEASURED APPROX 1.8 LONG. FAA FORM 8110-3 DATED 6/7/95, THE DAMAGE WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED.