What was found
INSPECTION FOUND A .50 INCH CRACK AT RIVET HOLE OF NR 1 ENGINE PYLON PANEL NR 5724. A 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 .50 INCH CRACK AT RIVET HOLE OF NR 1 ENGINE PYLON PANEL NR 5724. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.