What was found
LT FUSELAGE TO VERTICAL STAB ATTACH ANGLE IS CORRODED FROM THE REAR SPAR TO THE CENTER SPAR OF VERTICAL STAB. REPAIRED ATTACH ANGLE IAW SRM 53-2-5, 51-1-20D AND 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE TO VERTICAL STAB ATTACH ANGLE IS CORRODED FROM THE REAR SPAR TO THE CENTER SPAR OF VERTICAL STAB. REPAIRED ATTACH ANGLE IAW SRM 53-2-5, 51-1-20D AND 51-1-21.