What was found
A .25 INCH CRACK ON NR 4 ENGINE PYLON INBOARD SIDE GOING INTO SCREW ABOVE HORSE SHOE PLATE NACELLE STA 222. REPAIRED PER BOEING SRM 54-30-03 FIG 35.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .25 INCH CRACK ON NR 4 ENGINE PYLON INBOARD SIDE GOING INTO SCREW ABOVE HORSE SHOE PLATE NACELLE STA 222. REPAIRED PER BOEING SRM 54-30-03 FIG 35.