What was found
NR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.