What was found
DURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0.