What was found
INSPECTION FOUND A 1 CRACK IN NR 2 ENGINE TO PYLON UPPER AFT PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-10-2, 51-40-2, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 CRACK IN NR 2 ENGINE TO PYLON UPPER AFT PANEL. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-10-2, 51-40-2, AND 51-30-2.