What was found
INSPECTION FOUND A 1.5 INCH CRACK IN NR 2 ENGINE AFT NACELLE FIN (TRAILING EDGE FAIRING). THE TRAILING EDGE FAIRING CAP WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM'S 54-32-02, 54-12-02, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN NR 2 ENGINE AFT NACELLE FIN (TRAILING EDGE FAIRING). THE TRAILING EDGE FAIRING CAP WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM'S 54-32-02, 54-12-02, AND 51-31-01.