What was found
AT C-CHECK, NR 2 ENGINE RT T/R HALF CORE COWL INNER SURFACE FWD AREA CRACKED. CUT OUT CRACKED AREA PER CFM 56 MM, FABRICATED DOUBLER AND INSTALLED PER CFM 56 MM 78-31-10, 4 X 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, NR 2 ENGINE RT T/R HALF CORE COWL INNER SURFACE FWD AREA CRACKED. CUT OUT CRACKED AREA PER CFM 56 MM, FABRICATED DOUBLER AND INSTALLED PER CFM 56 MM 78-31-10, 4 X 3.