What was found
NR 1 ENGINE PYLON UPPER LEADING EDGE NR 8 RIB IS CRACKED. STOPPED DRILLED IAW SRM 54-50-1. REMOVED WEB IAW SRM 51-40-21 WELDING REPAIR IAW MAE T6/650912 INSTALLED WEB IAW 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE PYLON UPPER LEADING EDGE NR 8 RIB IS CRACKED. STOPPED DRILLED IAW SRM 54-50-1. REMOVED WEB IAW SRM 51-40-21 WELDING REPAIR IAW MAE T6/650912 INSTALLED WEB IAW 51-40-21.