What was found
VERTICAL STAB AFT DRAG ANGLE CRACKED ON LEFT SIDE. REPLACED THE DRAG ANGLE IAW SRM 51-42-00-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-40-06-001-001-A01, AND 51-42--22-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB AFT DRAG ANGLE CRACKED ON LEFT SIDE. REPLACED THE DRAG ANGLE IAW SRM 51-42-00-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-40-06-001-001-A01, AND 51-42--22-001-001-A01.