What was found
CRACKED ANGLE, INTERNAL STRUCTURE FRONT SPAR SUPPORT FITTING RT AREA APPROX AT BS 1016 IN THE VERTICAL STAB. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 176A3101, SHEET 4, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE, INTERNAL STRUCTURE FRONT SPAR SUPPORT FITTING RT AREA APPROX AT BS 1016 IN THE VERTICAL STAB. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 176A3101, SHEET 4, REV-.