What was found
CRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.