As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB FRONT SPAR FWD FACE ENTIRE LENGTH OF RT VERT STAB L/E HAS CORROSION UNDER NUT PLATES AND FASTENER HOLES. REMOVED CORROSION FROM RIB12-26 RT CHORD FLANGE CHECKED AND FOUND TO BE IN LIMITS IAW A310/200 SRM'S 51-74-10, 55-31-21.