As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT, THE FWD ENTRY DOOR LOWER HINGE CUT OUT WAS CRACKED, FWD 1 1/2 INCHES IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-01, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219, DETAIL III.