As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 99-215924 SECTION I. SECTION II REQUIRES REPETITIVE INSPECTIONS TO BE ACCOMPLISHED AT L-CHECK INTERVALS. SECTION III PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 3,000 CYCLES OR 24 MONTHS WHICHEVER COMES FIRST.