What was found
RIBS CRACKED AT VERTICAL STABILIZER LEADING EDGE RIGHT SIDE ZFS=50,43,23. RIBS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-2, 51-10-3 PAR 14-21, AND 55-02, FIG 27.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIBS CRACKED AT VERTICAL STABILIZER LEADING EDGE RIGHT SIDE ZFS=50,43,23. RIBS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-2, 51-10-3 PAR 14-21, AND 55-02, FIG 27.