What was found
INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT LEFT FAIRING SKIN AT AFT CORE COWL HINGE POINT. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, FIGURE 1 AND 54-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT LEFT FAIRING SKIN AT AFT CORE COWL HINGE POINT. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, FIGURE 1 AND 54-00-01.