What was found
FOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A.