What was found
LOWER FUSELAGE FRAME FWD WING TO FUSELAGE SUPPORT STRUCTURE FRAME IS CORRODED ALONG BOTTOM AROUND SCREW HOLES AT BS 661. BLENDED CORROSION, PERFORMED UT THICKNESS CHECK. COMPLIED WITH EA 30-2016-382.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE FRAME FWD WING TO FUSELAGE SUPPORT STRUCTURE FRAME IS CORRODED ALONG BOTTOM AROUND SCREW HOLES AT BS 661. BLENDED CORROSION, PERFORMED UT THICKNESS CHECK. COMPLIED WITH EA 30-2016-382.