What was found
AT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING LT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM LBL .5 TO LBL 1.5. STOP DRILLED CRACK, INSTALLED CHORD REPAIR PER AVITAS ENGINEERING DRAWING 96PMSI124R-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING LT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM LBL .5 TO LBL 1.5. STOP DRILLED CRACK, INSTALLED CHORD REPAIR PER AVITAS ENGINEERING DRAWING 96PMSI124R-1.