What was found
CRACK IN AFT MAIN CABIN FLOORBEAM ANGLE Y685.8 AT FRAME 86. REPLACED THE FLOORBEAM ANGLE IAW DRAWING 170-65660-447, AND SRM 51-41-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN AFT MAIN CABIN FLOORBEAM ANGLE Y685.8 AT FRAME 86. REPLACED THE FLOORBEAM ANGLE IAW DRAWING 170-65660-447, AND SRM 51-41-01.