What was found
DURING SCHEDULED 6Y CHECK, FOUND FLOOR PANEL T-ANGLE CRACKED AT BS 540, BETWEEN LBL 3 TO LBL 23. REMOVED AND REPLACED T-ANGLE PER SRM AND BAC DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 6Y CHECK, FOUND FLOOR PANEL T-ANGLE CRACKED AT BS 540, BETWEEN LBL 3 TO LBL 23. REMOVED AND REPLACED T-ANGLE PER SRM AND BAC DWG.