As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENG NOSE COWL AFT SIDE LOWER SUPPORT WEB ANGLE FOR STARTER VALVE WAS CRACKED. REMOVED CRACK SUPPORT ANGLE FROM NR 1 ENGINE AFT SIDE OF AFT BULKHEAD NOSE COWL IAW DC10 SRM 51-31-01 VOL 11. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW DC10 SRM 51-31-01 VOL 11. INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL11.