What was found
INSPECTION FOUND A 1 INCH CRACK ON WEB STIFFENER AND EXTERIOR SKIN OF NR 3 ENGINE PYLON AFT PANEL NR 488EL. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, 54-31-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK ON WEB STIFFENER AND EXTERIOR SKIN OF NR 3 ENGINE PYLON AFT PANEL NR 488EL. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, 54-31-01, AND 51-31-01.