As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED LONGERON NR 3LT AND 4LT, STA Y=160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGED SECTION OF LONGERONS 4LT AND 3LT WERE REMOVED AND NEW SECTIONS OF LONGERONS WERE INSTALLED. REPAIRS WERE IDENTIFIED IAW SRM 53-02, FIG 18 AND 51-10-4. RII COMPLETED.