What was found
Q1 CHECK - LEVEL 2 FRETTING CORROSION ON FUSELAGE TO VERTICAL STABILIZER LEFT FORWARD SUPPORT ANGLE INBOARD & OUTBOARD SIDES BETWEEN BS 1007 TO BS 1016, S3L+2 INCHES. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G, FIGS 2 & 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
Q1 CHECK - LEVEL 2 FRETTING CORROSION ON FUSELAGE TO VERTICAL STABILIZER LEFT FORWARD SUPPORT ANGLE INBOARD & OUTBOARD SIDES BETWEEN BS 1007 TO BS 1016, S3L+2 INCHES. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G, FIGS 2 & 8.