What was found
AT C-CHECK, NR 1 ENGINE FWD FIXED COWL AFT FRAME IS CRACKED AT LOWER END BY MOUNT BRACKET. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 4.5 X 2. N/R 6939.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, NR 1 ENGINE FWD FIXED COWL AFT FRAME IS CRACKED AT LOWER END BY MOUNT BRACKET. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 4.5 X 2. N/R 6939.