As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING RT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM RBL 1.5 TO 4.5. LOWER VERTICAL WEB CRACKED FROM RBL 1.25 TO 5.75. STOP DRILLED HOLES AND INSTALLED FIN FRONT SPAR FORGING AND WEB REPAIR PER AVITAS ENGINEERING DRAWING 96PMSI124D-1.