What was found
INSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.