What was found
MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE IS CORRODED FROM BS 940 - 947, RBL 56. R & R THE CREASE BEAM IAW DWG 147A8501, REV T, AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE IS CORRODED FROM BS 940 - 947, RBL 56. R & R THE CREASE BEAM IAW DWG 147A8501, REV T, AND SRM 51-40-02.