What was found
FOUND ON CV 2 CHECK 1 INCH CRACK IN LEADING EDGE SPAR STIFFENER AT NR 7 SLAT O/B TRACK O/B ANGLE. REPAIRED AND REPLACED STIFFNER PER M/M 57-20-21 PG 813.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ON CV 2 CHECK 1 INCH CRACK IN LEADING EDGE SPAR STIFFENER AT NR 7 SLAT O/B TRACK O/B ANGLE. REPAIRED AND REPLACED STIFFNER PER M/M 57-20-21 PG 813.