What was found
A 1 INCH CRACK AT NR 2 SLAT LWR COVE SKIN ANGLE O/B END. REPAIRED PER MM 57-54-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1 INCH CRACK AT NR 2 SLAT LWR COVE SKIN ANGLE O/B END. REPAIRED PER MM 57-54-0.