What was found
RIGHT AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1.5" LT AT FUSE TO VERTICAL CONNECTION. R & R RT AFT DRAG ANGLE IAW SRM 51-42-21-001-001-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.
RIGHT AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1.5" LT AT FUSE TO VERTICAL CONNECTION. R & R RT AFT DRAG ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.