What was found
RIGHT VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 & 51-42-00-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 & 51-42-00-001-001-A01.