As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C+SI SUSPECT CRACK IN FUSELAGE SKIN FROM FASTENER HOLE AT FWD UPPER CORNER OF FWD ENTRY DOOR CUT OUT. HEFC INSP CARRIED OUT IAW NDT MANUAL PT 6 51-00-00 FIG 4, CRACK CONFIRMED AND MEASURED AS 5MM IN LENGTH. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460C.