As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATIONS WERE NOTED AT THE NR 5 HOLE OF THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR (R1) CUT OUT AFT LWR CORNER DURING NDT INSP. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REPAIRED THE R1 DOOR AFT LOWER CORNER IAW SRM 53-10-61-2R-1, DETAIL II. (1469795)