What was found
FOUND DURING F-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING F-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0.