As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY REMOVED 2 AREAS OF CORROSION FROM RH WING AFT SPAR, FWD FACE IN RH MLG WHEEL WELL. EVALUATED AND FOUND BLENDED AREAS WERE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENDS IAW NETJETS ENGINEERING RFTS-113108, REV.0, TITLE: N323QS (680-0134) LH AND RH WING AFT SPAR CORROSION, DATE: 18MAR25.