What was found
CABIN FLOOR SUPPORT, UPPER ATTACH ANGLE WAS CRACKED AT BS 380+14, LBL 13. REMOVED & REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CABIN FLOOR SUPPORT, UPPER ATTACH ANGLE WAS CRACKED AT BS 380+14, LBL 13. REMOVED & REPLACED IAW SRM 51-40-02.