What was found
DURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT UPPER LEFT CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-209597 SECT I SECT II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT UPPER LEFT CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-209597 SECT I SECT II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT.