What was found
MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT APPROX STA 1575, RBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT APPROX STA 1575, RBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C.