As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY REMOVED 12 LARGE AREAS OF CORROSION LOCATED ON TAIL CONE SERVICE DOOR OUTER FRAME SKIN IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FOR NOMINAL THICKNESS IAW C680 SRM 51-70-02. REPAIRED CORROSION BLENDS IAW NETJETS ENGINEERING RFTS-113004 REV. 0 TITLE: N323QS (680-0134) TAILCONE SERVICE DOOR OUTER FRAME CORROSION DATE: 19FEB25