What was found
1/2-INCH CRACK IN LOWER INBOARD FLANGE RADIUS OF FORWARD SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER AT STA 00.000.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1/2-INCH CRACK IN LOWER INBOARD FLANGE RADIUS OF FORWARD SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER AT STA 00.000.