What was found
Q1 CHECK - LEVEL 2 FILIFORM CORROSION ON FUSELAGE TO VERTICAL STABILIZER LEFT AFT SUPPORT ANGLE INBOARD & OUTBOARD SIDES BETWEEN BS 1016 TO BS 1121, S3L. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
Q1 CHECK - LEVEL 2 FILIFORM CORROSION ON FUSELAGE TO VERTICAL STABILIZER LEFT AFT SUPPORT ANGLE INBOARD & OUTBOARD SIDES BETWEEN BS 1016 TO BS 1121, S3L. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G.