What was found
CRACK ON THE NACELLE REAR SECTION AT THE ANGLE BELOW THE FIREWALL ASSY. INSTALLED NR 2 ENGINE FIREWALL FLANGE IAW SRM 51-25-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON THE NACELLE REAR SECTION AT THE ANGLE BELOW THE FIREWALL ASSY. INSTALLED NR 2 ENGINE FIREWALL FLANGE IAW SRM 51-25-04.