What was found
DURING INSPECTION, THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE GOUGED INSIDE THE PYLON PANEL NR 414DB AT FRAME 67 & STRINGER 6LT. THE SKIN WAS REPAIRED IAW ETD 2014-145-031086.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE GOUGED INSIDE THE PYLON PANEL NR 414DB AT FRAME 67 & STRINGER 6LT. THE SKIN WAS REPAIRED IAW ETD 2014-145-031086.