What was found
CRACK ON LT ANGLE TO ATTACH VERTICAL STABILIZER INTERNAL BETWEEN, STA 1458-1486, LONGERON 1L - 2L. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942004.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT ANGLE TO ATTACH VERTICAL STABILIZER INTERNAL BETWEEN, STA 1458-1486, LONGERON 1L - 2L. ANGLE WAS REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05. LP 1942004.