As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF VERTICAL LEADING EDGE, FOUND VERTICAL STABILIZER SUPPORT FLANGE CRACKED ON RH SIDE JUST FORWARD OF PANEL 323GR. (C-CHECK RO 2/15/2025) REPAIRED VERTICAL STABILIZER FWD SPAR AT LEADING EDGE SUPPORT FLANGE WITH DOUBLER REPAIR REF ETD2025-170-000901 AND TI-170-25-003. SEE CONTINUE CARD FOR WORK PERFORMED. WEIGHT OF REPAIR DOES NOT CHANGE WEIGHT AND BALANCE OF AIRCRAFT.