What was found
INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR 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 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5430-01204.