What was found
MAIN CABIN FLOOR BEAM AT STA 246 HAS 1 EA VERTICAL STIFFENER ANGLE CRACKED AT LBL 50. REMOVED AND REPLACED CRACKED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR BEAM AT STA 246 HAS 1 EA VERTICAL STIFFENER ANGLE CRACKED AT LBL 50. REMOVED AND REPLACED CRACKED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV.