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 SKIN SURFACE AT 12 O'CLOCK POSITION JUST OUTBOARD OF INSPECTION PANEL HAS A 2" LONG CRACK RUNNING FROM RIVET HEAD. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-30-3 FIGURE 3 AND 3A.