What was found
NR 1 PYLON PANEL 413 CL HAS .50" GOUGE AT MILLED STIFFENER. COMPLIED WITH EA 6-5480-156100 NACELLES/ PYLONS INSTALLED REPAIR DOUBLER IAW SRM 54-52-51, FIG 202, SHEET 1, PGS 209-210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 PYLON PANEL 413 CL HAS .50" GOUGE AT MILLED STIFFENER. COMPLIED WITH EA 6-5480-156100 NACELLES/ PYLONS INSTALLED REPAIR DOUBLER IAW SRM 54-52-51, FIG 202, SHEET 1, PGS 209-210.