What was found
NR 1 ENGINE EXHAUST NOZZLE 436AL ACCESS PANEL CAM LOCK SOCKET STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE EXHAUST NOZZLE 436AL ACCESS PANEL CAM LOCK SOCKET STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM 51-42-06.