What was found
SMALL AREA OF CORROSION ON FUSELAGE SKIN AT FRAME 35 BETWEEN STRINGERS 20 - 21L. C-CHECK, CUTOUT AND REMOVED SKIN CORROSION AND INSTALLED FILLER WITH EXTERNAL DOUBLER IAW ETD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SMALL AREA OF CORROSION ON FUSELAGE SKIN AT FRAME 35 BETWEEN STRINGERS 20 - 21L. C-CHECK, CUTOUT AND REMOVED SKIN CORROSION AND INSTALLED FILLER WITH EXTERNAL DOUBLER IAW ETD.