What was found
A .5 INCH VISABLE CRACK O/B END NR 2 SLAT IN COVE SKIN ATTACH ANGLE. REPAIR PER M/M 57-54-000-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .5 INCH VISABLE CRACK O/B END NR 2 SLAT IN COVE SKIN ATTACH ANGLE. REPAIR PER M/M 57-54-000-8.