As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK, NR 1 ENGINE PYLON LT AFT REVERSER COWL UPPER AFT AREA FOUND CRACK ON U-CHANNEL ANGLE. REMOVED CRACKED U-CHANNEL ANGLE AT ENG NR 1 LT AFT REVERSER COWL IAW DC-8 SRM 51-1-21A PG 1 PARA 1. FABRICATED NEW U ANGLE 5.5 X 1.375. 301 STAINLESS .25 HARD 0.20. IAW DC-8 SRM 51-1-7 PG 1 PARA 1. INSTALLED U-CHANNEL ANGLE PER DC-8 SRM 51-1-21 PG 1 PARA 1.