What was found
RT TAIL CONE AFT DRAG ANGLE IS CRACKED ON FWD END. INSTALLED RT AFT TAIL CONE AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT TAIL CONE AFT DRAG ANGLE IS CRACKED ON FWD END. INSTALLED RT AFT TAIL CONE AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01.