What was found
INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.