As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT FORWARD UPPER CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-209598 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE 2 YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT.