What was found
CRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER L/E INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW SRM 55-02D, FIG 27.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER L/E INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW SRM 55-02D, FIG 27.