What was found
RT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND CRACKED. DRAG ANGLE WAS REPAIRED IAW EA 16-2013-042. COMPLIED WITH HFEC INSPECTION. REINSTALLED ACCES SKIN PANEL IAW RD8-51-0015 AND SRM 51-42-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND CRACKED. DRAG ANGLE WAS REPAIRED IAW EA 16-2013-042. COMPLIED WITH HFEC INSPECTION. REINSTALLED ACCES SKIN PANEL IAW RD8-51-0015 AND SRM 51-42-05.