As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE IS BENT OUT AND 1" CRACK. CUT OUT DAMAGE AREA DIMENSION 2" BY .75" IAW SRM 51-10-1. FABRICATED NEW DOUBLER REPAIR IAW SRM 51-30-5 AND 54-30-2 FIG 1. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 54-30-3 FIG 8 AND 51-30-2 ON NR 1 ENGINE NOSE COWL EXTERIOR SKIN TRAILING EDGE 9 O'CLOCK POSITION.