As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE INLET COWL INNER SUPPORT BRACKETS ARE CRACKED AT 6 OCLOCK POSITION CUT OUT DAMAGED AREA. FABRICATED FRAME SECTION USING 2024T-3 .063 DIMS 6 5/8" X 2 1/4" AND STRAP REPAIR USING 2024T-3 .071 DIMS 13 1/4" X 1 1/4" AND INSTALLED ALL REPAIR PARTS IAW SRM 54-10-3.