What was found
CRACK ON LT/RT INTERNAL VERTIACL STABILIZER ATTACH DORSAL ANGLES BETWEEN STA Y=1458 TO 1486. DORSAL ANGLES WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT/RT INTERNAL VERTIACL STABILIZER ATTACH DORSAL ANGLES BETWEEN STA Y=1458 TO 1486. DORSAL ANGLES WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05.