As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE REMOVAL OF THE KA BAND-RADOME STRUCTURAL PROVISIONS AS PER SB 190-53-0125, WAS FOUND THE FUSELAGE SKIN WITH CORROSION AROUND THE EXISTING HOLE CUT OUT BETWEEN FRAME 63 AND 64 AND BETWEEN STRINGER 01L AND 02L. DUE TO THIS SITUATION WAS REPAIRED IAW EMB ETD2025-190-902178 AND COOPESA ENGINEERING ORDER COO-EO-2025-21781 DTD FEB 21 2025