What was found
INSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.