As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED .625 INCH CRACK SIX INCHES FORWARD OF L-1 DOOR IN FUSELAGE SKIN AT STRINGER 7. MAINTENANCE REPAIRED CRACK PER SRM 53-30-3, PAGES 7 AND 8. (M)