What was found
NR 2 NACELLE OTBD LOWER ENGINE SUPPORT STRUT CHAFED AT THE OIL COOLER RETURN LINE, MEASURED AT 0.012". REPAIRED IAW RD8-54-1264. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 NACELLE OTBD LOWER ENGINE SUPPORT STRUT CHAFED AT THE OIL COOLER RETURN LINE, MEASURED AT 0.012". REPAIRED IAW RD8-54-1264. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED.