What was found
A .75 INCH CRACK NR 3 SLAT O/B TRACK VERTICAL STIFFENER ON WING FRONT SPAR. REPLACED ANGLE PER M/M 57-20-21 NR 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .75 INCH CRACK NR 3 SLAT O/B TRACK VERTICAL STIFFENER ON WING FRONT SPAR. REPLACED ANGLE PER M/M 57-20-21 NR 14.