As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT SIDE; VERTICAL FIN SKATE ANGEL; WORN/CHAFFING; STA. 1119-1127. / REMOVED DAMAGE FROM RT VERTICAL FIN SKATE ANGLE IAW SRM 51-10-02-0G-0 ORIG THICKNESS .063' LOSS OF .001' REMAINING .062' FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM ALLOWABLES FOR THE CLOSURE ANGLE REPAIRED SKATE ANGLE AT STA 1119-1127 IAW EA 210016 IR AND SWA EA 21-153-00125 REV IR