What was found
CRACKED RIB ON VERTICAL STABILIZER INTERNAL STRUCTURE STA ZFS=4.7 AND ZFS=17. RIBS WERE REPAIRED PER SRM 55-02 FIG 27, 51-30-2, 51-30-5 AND 51-10-3 PAR. 14, 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED RIB ON VERTICAL STABILIZER INTERNAL STRUCTURE STA ZFS=4.7 AND ZFS=17. RIBS WERE REPAIRED PER SRM 55-02 FIG 27, 51-30-2, 51-30-5 AND 51-10-3 PAR. 14, 21.