What was found
INSPECTION FOUND A .5 INCH CRACK IN NR 1 I/B PYLON SKIN AT FORWARD UPPER CORNER OF PANEL 5724. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN NR 1 I/B PYLON SKIN AT FORWARD UPPER CORNER OF PANEL 5724. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204.