What was found
DURING F-1 LETTER CHECK, FOUND .375 INCH CRACK AND 1 INCH CRACK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. 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 .375 INCH CRACK AND 1 INCH CRACK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.