What was found
INSPECTION FOUND A .5 INCH CRACK AT O/B FORWARD CORNER OF NR 1 ENGINE PYLON ACCESS PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5340-01230.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT O/B FORWARD CORNER OF NR 1 ENGINE PYLON ACCESS PANEL 5727L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5340-01230.