What was found
FORWARD CABIN FUSELAGE FLOOR PANEL ANGLE HAS CORROSION AT X= FRAME 14, Y=711.2. R & R FLOOR PANEL ANGLE 170-04075-001 IAW SRM 51-43-01, WO 1468092 1G9 & EO E175-5300-101 REV IR WO 1834324.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD CABIN FUSELAGE FLOOR PANEL ANGLE HAS CORROSION AT X= FRAME 14, Y=711.2. R & R FLOOR PANEL ANGLE 170-04075-001 IAW SRM 51-43-01, WO 1468092 1G9 & EO E175-5300-101 REV IR WO 1834324.