What was found
C2 PDX - NACELLE FORWARD FRAME ASSEMBLY GOUGED/GALLED NEAR LOWER COWL ATTACH POINT, LEFT SIDE, NR 1 ENGINE. REPAIRED IAW SRM 51-14-00 AND RD8/4-54-388.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C2 PDX - NACELLE FORWARD FRAME ASSEMBLY GOUGED/GALLED NEAR LOWER COWL ATTACH POINT, LEFT SIDE, NR 1 ENGINE. REPAIRED IAW SRM 51-14-00 AND RD8/4-54-388.