What was found
MAIN CABIN CREASE BEAM INBD ANGLE HAS AREAS OF CORROSION BETWEEN BS 680 - 740. REMOVED CORROSION FROM CREASE BEAM ANGLE IAW SRM 53-00-51. REMAINING MATERIAL THICKNESS AFTER CORROSION REMOVAL FOUND TO BE WITHIN LIMITS IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN CREASE BEAM INBD ANGLE HAS AREAS OF CORROSION BETWEEN BS 680 - 740. REMOVED CORROSION FROM CREASE BEAM ANGLE IAW SRM 53-00-51. REMAINING MATERIAL THICKNESS AFTER CORROSION REMOVAL FOUND TO BE WITHIN LIMITS IAW SRM.