What was found
VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-77-00-001-001-A01, 51-40-11-001-001-A01, 51-25-01-001-001-A01 TR 51-0055.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-77-00-001-001-A01, 51-40-11-001-001-A01, 51-25-01-001-001-A01 TR 51-0055.