As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY MAINTENANCE, CRACK ON END AREA OF STRINGER 9LH AT FUSELAGE STRUCTURE FRAME 91; REF TOMX WO 1834 NR -00468, STRINGER 9LH AT FUSELAGE STRUCTURE FRAME 91 WAS REPLACED FOR A NEW STRINGER PER EMB-190 SRM 51-41-02 AND SRM 51-43-03