As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE INTERIOR FRAME AT RIGHT STA 1681 LONGERON 11 FOUND DAMAGED. UPPER FUSELAGE INTERIOR, DENT FRAME AT RT BS 1681 LONGERON 11 REPAIRED AS PER SRM 53-30-00. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.