As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING "L" CHECK FOUND CRACKS IN FUSELAGE SKIN AT FORWARD UPPER CORNER OF FORWARD PASSENGER DOOR JAMB. REPAIRED PER EA 98-210174 SECT I. SECTION II INSPECTION TO BE PERFORMED EVERY 3000 CYCLES. PERMANENT REPAIR PER SECTION III TO BE ACCOMPLISHED ON OR BEFORE 2 YEARS/24 MONTHS AFTER SECTION I ACCOMPLISHMENT.