As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CORROSION AT STA. 1720 AND STRINGER 42 RIGHT(<P ><SPAN>AREA OF CORROSION WAS CUT OUT, NO CORROSION WAS FOUND ON THE STRINGER. HFEC WAS ACCOMPLISHED AROUND CUT OUT AND EXISTING HOLES WITH NO FINDINGS. ORIGINAL SKIN WAS 2024-T3 .080". DOUBLER WAS FABRICATED FROM 2024 T3 .090" AND INSTALLED WITH .080 FILLER.</SPAN></P> / <P> </P>)