As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OP 16 MAINT CHECK, THE FWD ENTRY DOOR LOWER HINGE CUT-OUT WAS CRACKED OUT, FWD 1.5 IN LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219, DETAIL III.