What was found
INSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1/2" CRACK IN #2 ENGINE UPPER PYLON SKIN AT ACCESS PANEL 5827R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.