What was found
A .5 INCH CRACK IN I/B ATTACH ANGLE/ SPAR STIFFENER FOR NR 4 SLAT ACT. REPLACED STIFFENER PER 57-20-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .5 INCH CRACK IN I/B ATTACH ANGLE/ SPAR STIFFENER FOR NR 4 SLAT ACT. REPLACED STIFFENER PER 57-20-21.