What was found
DURING "H" CHECK, FOUND CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF FORWARD SERVICE DOOR JAMB . REPAIRED PER EA 99-209601 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3,000 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 FUSELAGE SKIN AT AFT UPPER CORNER OF FORWARD SERVICE DOOR JAMB . REPAIRED PER EA 99-209601 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3,000 CYCLES AFTER SECTION I ACCOMPLISHMENT.