What was found
MAIN CABIN BS 860 - 870 LBL 89 FLOORBEAM L-ANGLE BETWEEN UPPER CHORD TO SEAT TRACK CRACKED. C-CHECK. REPLACED L-ANGLE, REF SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN BS 860 - 870 LBL 89 FLOORBEAM L-ANGLE BETWEEN UPPER CHORD TO SEAT TRACK CRACKED. C-CHECK. REPLACED L-ANGLE, REF SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.