As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE NOSE COWL EXTERIOR AFT BACKSIDE BULKHEAD I/B AT 5 O'CLOCK POSITION VERTICAL ANGLE STIFFENER SUPPORT IS CRACKED AT TOP END REMOVED VERTICAL STIFFENER NR 1 ENG NOSE COWL AFT AT 5 O'CLOCK BULKHEAD IAW SRM REV 103 51-30-2 FABRICATED NEW STIFFENER FROM 2024T3 .040" DIM 6" X 3" IAW SRM 51-20-1 FIG 7 INSTALLED STIFFENER IAW SRM 51-30-2 REV 103