What was found
MAIN CABIN FLOOR SUPPORT UPPER ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1260 - 1280, BL 0, REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR SUPPORT UPPER ANGLE HAS CRACKS AROUND FASTENER HOLES BETWEEN BS 1260 - 1280, BL 0, REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM 51-40-02, PAR 4, AND 51-40-05, FIG 2.