What was found
VERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.