What was found
A 2 INCH CRACK AT WING L/E FRONT SPAR STIFFENER AT NR 6 SLAT O/B TRACK-O/B STIFFENER. REPAIR PER M/M 57-20-021-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 2 INCH CRACK AT WING L/E FRONT SPAR STIFFENER AT NR 6 SLAT O/B TRACK-O/B STIFFENER. REPAIR PER M/M 57-20-021-8.