What was found
LT VERTICAL AFT DRAG ANGLE CRACKED. REMOVED THE DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-10-001-01-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01 AND DWG BA670-35002.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT VERTICAL AFT DRAG ANGLE CRACKED. REMOVED THE DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-10-001-01-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01 AND DWG BA670-35002.