What was found
INSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.