What was found
A .25 INCH VISIBLE CRACK I/B OF STOP PAD NR 8 SLAT COVE SKIN ATTACH ANGLE. REPAIR PER MM 57-54-000-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .25 INCH VISIBLE CRACK I/B OF STOP PAD NR 8 SLAT COVE SKIN ATTACH ANGLE. REPAIR PER MM 57-54-000-8.