What was found
INSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.