As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PDX - C5 - THE RT INBD FWD ATTACH ANGLE FOR THE SPINE COWL ON THE NR 1 ENGINE NACELLE IS CRACKED. REMOVED NR 1 ENGINE INBOARD FWD ATTACH ANGLE FOR THE SPINE COWL IAW SRM 51-42-05-2-01 PARA 4E. FABRICATED NEW NR 1 ENGINE RT INBD FWD ATTACH ANGLE FOR THE SPINE COWL IAW RD 8/4-71-032. INSTALLED ANGLE IAW RD 8/4-71-032.