What was found
INSPECTION FOUND A 1/4 INCH CRACK IN NR 2 OB PYLON SKIN AFT OF UPPER T/R ABOVE PANEL 5824R. A DOUBLER AND FREEZE PLUGS WERE INSTALLED IAW SRM 5450-01330 AND ECRA 5430-01204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/4 INCH CRACK IN NR 2 OB PYLON SKIN AFT OF UPPER T/R ABOVE PANEL 5824R. A DOUBLER AND FREEZE PLUGS WERE INSTALLED IAW SRM 5450-01330 AND ECRA 5430-01204.