As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT C CHECK, NR 1 ENGINE UPPER COWL O/B EDGE IS WORN THRU BETWEEN NR 2 AND NR 3 COWL LATCHES. REMOVED AND REPLACED ANGLE AT NR 1 ENG UPPER COWL O/B EDGE BETWEEN NR 2 AND NR 3 COWL LATCHES PER B727 SRM 51-30-2 MAT USED .030 2024T3 24.5 X 4, TREATED AND PRIMED U ANGLE PER B727 SRM 51-10-2. N/R 6372.