What was found
LEFT VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED & 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, AND 51-25-01-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED & 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, AND 51-25-01-001-001-A01.